Author: Ramkumar Sundarakalatharan

Cracking The Secret Codes Of The European Galileo Satellite Network

Cracking The Secret Codes Of The European Galileo Satellite Network

Mark Psiaki, left, professor of mechanical and aerospace engineering, hooks up an experimental GPS/Galileo digital storage receiver and patch antenna with the assistance of graduate students Todd Humphreys, center, and Shan Mohiuddin in Rhodes Hall. by Staff WritersIthaca NY (SPX) Jul 19, 2006Members of Cornell’s Global Positioning System Laboratory have cracked the so-called pseudo random number codes of Europe’s first global navigation satellite, despite efforts to keep the codes secret. That means free access for consumers who use navigation devices – including handheld receivers and systems installed in vehicles – that need PRNs to listen to satellites.The codes and the methods used to extract them were published in the June issue of GPS World.
The navigational satellite, called the GIOVE-A, for Galileo In-Orbit Validation Element-A, is a prototype for 30 satellites that by 2010 will constitute Galileo, a $4-billion joint venture of the European Union, European Space Agency and private investors. Galileo is Europe’s answer to the U.S. GPS system.
Because GPS satellites, which were put into orbit by the Department of Defense, are funded by U.S. taxpayers, the signal is free — consumers need only purchase a receiver. Galileo, on the other hand, must make money to reimburse its investors — presumably by charging a fee for PRN codes.
Because Galileo and GPS will share frequency bandwidths, Europe and the United States signed an agreement whereby some of Galileo’s PRN codes must be “open source.” Nevertheless, after broadcasting its first signals on Jan. 12, 2006, none of GIOVE-A’s codes had been made public.
In late January, Mark Psiaki, an aerospace engineer at Cornell and co-leader of the GPS Laboratory, requested the codes from Martin Unwin at Surrey Satellite Technology Ltd., one of three privileged groups in the world with the PRN codes.
“In a very polite way, he said, ‘Sorry, goodbye,'” recalled Psiaki. Next, Psiaki contacted Oliver Montenbruck, a friend and colleague in Germany, and discovered that he also wanted the codes. “Even Europeans were being frustrated,” said Psiaki. “Then it dawned on me: Maybe we can pull these things off the air, just with an antenna and lots of signal processing.”
Within one week Psiaki’s team developed a basic algorithm to extract the codes. Two weeks later they had their first signal from the satellite, but were thrown off track because the signal’s repeat period was twice that expected. By mid-March they derived their first estimates of the code, and — with clever detective work and an important tip from Montenbruck — published final versions on their Web site on April 1. Two days later, NovAtel Inc., a Canadian-based major manufacturer of GPS receivers, downloaded the codes from the Web site in a few minutes and soon afterward began tracking GIOVE-A for the first time.
Galileo eventually published PRN codes in mid-April, but they weren’t the codes currently used by the GIOVE-A satellite. Furthermore, the same publication labeled the open source codes as intellectual property, claiming a license is required for any commercial receiver. “That caught my eye right away,” said Psiaki. “Apparently they were trying to make money on the open source code.”
Afraid that cracking the code might have been copyright infringement, Psiaki’s group sought outside help. “We were told that cracking the encryption of creative content, like music or a movie, is illegal, but the encryption used by a navigation signal is fair game,” said Psiaki. The upshot: The Europeans cannot copyright basic data about the physical world, even if the data are coming from a satellite that they built.
“Imagine someone builds a lighthouse,” argued Psiaki. “And I’ve gone by and see how often the light flashes and measured where the coordinates are. Can the owner charge me a licensing fee for looking at the light? … No. How is looking at the Galileo satellite any different?”
Other authors of the GPS World article are Cornell colleagues Paul Kintner, Todd Humphreys, Shan Mohiuddin, Alessandro Cerruti and Steven Powell

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New Horizons Crosses The Asteroid Belt

New Horizons Crosses The Asteroid Belt

New Horizons Crosses The Asteroid Belt

New Horizons has entered the main asteroid belt and will be traversing this part of our solar system through August. May, like April, was a busy month for New Horizons’ instrument payload commissioning. In particular, our instruments LORRI, PEPSSI, Alice and Ralph all continued their in in-flight checkouts.In addition, the spacecraft itself received a new suite of onboard fault-protection autonomy software, resolving a number of needed bug fixes discovered in ground and flight testing.
We continue to see software-induced guidance computer resets once or twice per month on average, but the spacecraft recovers flawlessly from these, without any interruption to plans. New software for this computer is in the works and will resolve the bug that causes this; we expect to have it tested and aboard the spacecraft around Oct. 1.
Highlights of our payload-commissioning activities included door openings for PEPSSI (May 3), Alice (May 20) and Ralph (May 29). The Student Dust Counter registered each of these events at the precise time of the door openings by the noise they made on the spacecraft.
Each of these instruments also saw first light, i.e., detecting signals from stars (Ralph) or the interplanetary medium (PEPSSI and Alice). From these tests we appear to have a little higher-than-spec sensitivity with Ralph’s color and panchromatic cameras.
We also found that Alice’s background counts are only about half of what we predicted, indicating the RTG induces a significantly lower background than we estimated before launch. This lower background rate will substantially enhance Alice’s signal-to-noise ratio on faint spectral features.
From the Alice, Ralph, and PEPSSI testing this month, we can continue to say, from all of the data surrounding the careful, step-by-step instrument-commissioning activities to date, that our instrument payload continues to look like it’s performing as well or better than predicted from ground testing. This is a testament to the exacting engineering that went into their development.
In other news for May, we began to finalize the suite of Jupiter observations planned for next year during our Jupiter flyby, and we continued to track New Horizons to determine whether a fine course correction will be needed this fall. So far, none appears necessary, but the final verdict won’t be in until we have about another 90 to 100 days of tracking.
Planning activities began in May for the 60 day checkouts we’ll perform each year during Cruise 2, also known as Glen’s Glide: the coast from Jupiter to Pluto.
From 2008 to 2011, these checkouts will occur in the fall of each year, but in 2012, 2013 and 2014 the checkouts will occur in the summer. The summertime checkouts will occur in 2012 and 2014 because we’ll be rehearsing the Pluto encounter aboard the spacecraft during these checkouts, and we want the Earth-Sun geometry at rehearsal time to reproduce faithfully what will occur at the encounter, in the summer of 2015. The 2013 checkout provides a backup opportunity for an additional rehearsal if one becomes necessary.
I’ll now turn to the “water cooler news story” of the month for New Horizons: In early May, we got word from Lockheed-Martin that tourists in the Bahamas found several large pieces of our Atlas V 551 launch vehicle’s nose fairing that had washed up on shore.
Now, turn to the significance of our current location: deep in the solar system’s main asteroid belt. This region comprises a handful of dwarf planets, such as Ceres – itself 1,000 kilometers (620 miles) in diameter – and literally millions of debris bits created by collisions between asteroids.
These small bodies range in size from mountains to objects as large as 100 kilometers (62 miles) across. The asteroid belt also contains innumerable boulders, rocks and dust motes created by the same collisions.
The first spacecraft to transit the asteroid belt was NASA’s Pioneer 10, which made its epic crossing in 1972 on the way to the historic first encounter of a spacecraft with Jupiter.
Later, Pioneer 11, Voyagers 1 and 2, Galileo, Cassini, NEAR and Ulysses have all made the same kind of journey across the main belt. Now it is our turn.
Fortunately, the asteroid belt is so huge that, despite its large population of small bodies, the chance of running into one is almost vanishingly small – far less than one in a billion. That means if you want to come close enough to an asteroid to make detailed studies of it, you have to aim for one.
The first such asteroid flyby was made by Galileo in October 1991, and Galileo made a second asteroid encounter in 1994.
Other spacecraft, most notably the NEAR (Near Earth Asteroid Rendezvous) mission, also have made close main-belt-asteroid flybys, yielding important geological and geophysical insights into these bodies.
Galileo made the first discovery of an asteroid satellite in its 1991 flyby of Gaspra. Since then, ground-based observers have found dozens of asteroid satellites.
In addition to main belt asteroid flybys, NASA’s NEAR and the Japanese Hayabusa mission both have made orbital rendezvous and landings on asteroids closer to Earth.
Next year, NASA plans to launch the Dawn Discovery mission to orbit two of the largest asteroids: Vesta and Ceres. Dawn will arrive in orbit about Vesta in 2012, and will reach Ceres, the largest asteroid, in August 2015, just a month or so after New Horizons encounters Pluto.
A long time ago, we considered the possibility of targeting a close asteroid flyby with New Horizons during our main belt traverse. As the mission’s principal investigator, I rejected this early on for two reasons.
First, such an encounter would take about half of our Kuiper Belt fuel to accomplish. Second, even for this amount of fuel, the only asteroids we could hope to reach would be tiny – just a few kilometers across.
Though such an encounter certainly would be scientifically useful, it couldn’t be justified for the amount of fuel it would cost us – after all, our job is to reconnoiter bodies in the Kuiper belt with that fuel, not the asteroid belt.
As a result, we specifically decided not to target any asteroid, but after launch we did conduct a thorough search for chance encounters along our trajectory. Just the statistics of such chance encounters indicated that we might expect to pass perhaps 1 million to 3 million kilometers (620,000 to 1.8 million miles) from a small asteroid by chance as we transited the main belt. We found several such opportunities back in February.
As it turned out, we got more than what we expected: In early May we also discovered we’d pass within just 104,000 kilometers (63,000 miles) of the little-known asteroid 2002 JF56 on June 13. This little mountain-sized body is only 3 kilometers to 5 kilometers (1.9 miles to 3.1 miles) across, and virtually nothing is known about it – not even its compositional type or rotational period.
We cannot resolve something as small as 2002 JF56 from this distance with Ralph (LORRI, which has higher resolution cannot open its door until late August to guard against accidental Sun pointings), but the June 13 encounter with 2002 JF56 is still going to be useful to New Horizons.
The primary use of this distant flyby will be to test Ralph’s optical navigation and moving-target tracking capabilities. We also will be able to get a handle on the asteroid’s light curve, composition, phase curve, and perhaps even refine its diameter, if all goes as planned.
The event is really a flight test, so we aren’t guaranteeing anything but a best effort. If it works, you’ll see images that just barely resolve the asteroid into perhaps one or two pixels and perhaps a spectrum of this chip off some larger body.
More important, of course, we will gain some valuable experience that will yield benefits at both the Jupiter and Pluto flybys, so we’re excited to give this a try. Stay tuned, we’ll report on the results at mid-month on our Web site.
Other flight
activities for June will center on SWAP instrument testing, Ralph instrument calibrations and beam-mapping observations for our high gain antenna and REX (radio science) instrument.
By July Fourth, we’ll be 3 AU from the Sun. Although the sunlight there is still 100 times as strong as it is on the brightest day at Pluto, it’ll be about 10 times dimmer than at Earth’s orbit. Less than six months into a 114 month journey to Pluto, New Horizons is beginning to reach the cooler thermal conditions it was designed to thrive in!
That’s all I have for now. So, until next time, keep exploring.

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ISRO And DRDO Deal Differently With Disastrous Launches

ISRO And DRDO Deal Differently With Disastrous Launches

ISRO And DRDO Deal Differently With Disastrous Launches
File photo: The doomed Agni-III missile.by Staff WritersNew Delhi, India (PTI) Jul 18, 2006It was a Black Sunday and an even worse Monday for India’s aerospace ambitions. Two much-hyped rocket systems – one the guided missile Agni-III, and another the GSLV-FO2 launch vehicle carrying a satellite – built by two famed institutions, (RDO and ISRO, landed in the sea, drowning with them years of effort and hundreds of crores of rupees.

It was a rare back-to-back failure and ISRO chairman Madhavan Nair was forthright on what could have gone wrong: “The pressure in one of the four strap-on motors dropped to zero and did not develop enough thrust, as a result the vehicle veered off the trajectory,” he said, adding that the failure was “a rarest phenomena”.

“One of the liquid strap-ons had a workmanship problem with the engine valve, leading to a shutdown after one second,” a source revealed.

Unlike ISRO, who even after the failure showed a genuine eagerness to share available information, there was total silence from the DRDO. An indifferent defense minister summed up the situation: “The take-off was successful … but there was some problem later.”
Repeated efforts to talk to DRDO officials in Hyderabad met with no success, though one scientist did say there could have been a “component flaw, but even that would be premature to say”.

ISRO and DRDO are studies in contrast, two high-profile organizations heavily funded by public money and trying to meet India’s goals of self-reliance in critical technology. The difference is one seems to have learned from its failures and has a brilliant track record, while the other seems lost.

Much of ISRO’s talent and innovation has been used by DRDO for its missile program, “but the spirit and resilience of ISRO was never transferred to DRDO even though conceptually there is proximity between the two,” said a scientist who has worked in both organizations.
What makes ISRO different? “The one great thing about ISRO is that it is extremely open, people are committed, they have faith in themselves and a failure is seen as a learning curve. Our reviews are open,” said ex-ISRO chairman U.R. Rao.

“Nowhere in the world will you find another organization like ISRO,” said another official. “Everything is done here from end to end. We do R&D; build satellites and launch vehicles; meet the specific requirements of our users and also process data.”
Of the 21 launches ISRO has attempted in India, only five have failed, the last in April 1994. This is a highly respected success rate, even globally. At DRDO, however, the missile program has been the only effort that has met with some success.

Now, with Agni-III’s failure, the Integrated Guided Missile Program, which began in 1983, has suffered a major setback. The Agni test, said DRDO sources, was supposed to give a technical push to the intercontinental missile program.

“DRDO has got into the problem of talking big and delivering little,” said a scientist, recalling how in 2003 the much touted short-range surface-to-air missile Trishul was dumped. DRDO had worked on it for 18 years and spent nearly Rs 300 crore. Other missiles in the IGM program – Akash and Nag (promised long ago and yet to be delivered) – already have consumed thousands of crores.

It is ironic the DRDO was set up to cut down on arms imports via indigenization. A few years ago, President A.P.J. Abdul Kalam had spoken of 70 percent self-reliance in defense requirements by 2005. That date and year have passed, and India is still a long way away from that goal.

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China To Develop Deep Space Exploration In 5 Years

China To Develop Deep Space Exploration In 5 Years

China To Develop Deep Space Exploration In 5 Years
China hopes to send its spacecraft beyond the moon
Beijing, China (SPX) Jul 20, 2006
A senior Chinese space agency official said Wednesday that China would actively plan its deep space exploration over the next five years, focusing on lunar and Mars exploration.

Sun Laiyan, administrator of the China National Space Administration, said China would study the distribution and utilization of lunar resources and terrestrial planetary science as well as exploring scientific measures for supporting mankind’s sustainable survival on Earth.

Key research areas will also include astronomy and solar physics, space physics and solar system exploration, micro-gravity sciences and space life science.
Sun urged Chinese scientists to increase their understanding of star and universe evolution through the observation and study of the sun and black holes.

In the next five years, Sun said, China will independently develop and launch an astronomical satellite.

China will advance its exploration of the integral behavior of the chain reaction of solar-terrestrial space, establish a space weather forecast pattern on which a weather support system for space flight safety and communication will be based, he told the 36th Scientific Assembly of the Committee on Space Research.

Sun said, “Priorities shall be given to innovative projects on major scientific problems, and the emphases will be laid on Sun-Earth space environment study, solar system exploration and space astronomy.”

Sun’s administration is striving to establish an open, fair and scientific competition system for the selection of all space science projects, he said.
“We need to avoid unorganized competition by publicly collecting and evaluating proposals, and carrying out feasibility studies,” Sun said.

“We’ll also encourage and support other countries to join in the programs initiated by China in space science, and Chinese scientists will participate in international space science programs,” the administrator said.

During the 11th Five-Year (2006-2010) Program period, research into micro-gravity science will be coordinated with national scientific and technological strategic objectives.
This will promote the development of high technology for biological engineering and new materials and basic research on gravity theory and life science.

Chinese scientists have already conducted space experiments in astronomy, environment, microgravity fluid physics, material science, life science and earth science.
In February 2004, China initiated the Lunar Exploration Mission and started the research and development of the Chang’e lunar probe.

In October 2005, Shenzhou VI for the first time operated manned space lab experiments. China also launched four recoverable satellites.The results achieved through many years of research have laid a foundation for the fulfillment of space science development goals set out in the 11th Five-Year Program. After over ten years of advanced research on Space Solar Telescope and Space Hard X-Ray Modulation Telescope, scientists have tackled problems on key technologies and manufactured models of main components.

It is estimated that in the past decade, China’s space science investment, including infrastructure and programs, had exceeded 900 million yuan ($112.5 million).
The National High-Tech Research and Development Program initiated in the mid 1980s and the Manned Space flight Program begun in 1992 substantially promoted the development of China’s space research.

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GSLV Failure, Yes this does happen., Now & then

GSLV Failure, Yes this does happen., Now & then

The Official Press Release from the ISRO is below and it describes that the GSLV “cannot complete its mission” ie. putting the satelitte on orbit. But, as it came to know the Liquid strap-ons were (seems to be ) the reason for this hitch too., (as was in 1999).

PRESS RELEASE
Date Released: Monday, July 10, 2006
Source: Indian Space Research Organisation
India’s Geosynchronous Satellite Launch Vehicle (GSLV-F02), with INSAT-4C on board, was launched from Satish Dhawan Space Centre SHAR (SDSC SHAR), Sriharihota today (July 10, 2006).

The lift-off took place at 5:38 p.m. IST.
However, GSLV-F02 could not complete the mission.

The detailed analysis of the data received from the vehicle is being analysed to pinpoint the exact reasons.

The Anatomy of the ” Failure “
The second operational flight of the GSLV rocket that was to hurl the country’s heaviest satellite yet built , 36,000 km into space instead plunged into the sea, within a minute of launch from the country’s space port at Sriharikota.
One of the four strap-on motors, attached to the 49-metre-tall, 414 tonne GSLV did not give the required thrust forcing the rocket to deviate from its flight path by about 10 degrees. The project director, who found that the first stage did not separate from the upper two stages, pressed the button to destroy the rocket for safety reasons. “It appears from preliminary data that the pressure had dropped to zero in one of the four strap-on motors and it failed to give the required thrust to the GSLV,” Indian Space Research Organisation (ISRO) Chairman G Madhavan Nair said, after the mishap, the first major incident in 12 launches of the space agency.(considering 9 Succesful launches in Row with 6 Foreign Satelittes/Payloads)
Five years ago, the first experimental GSLV rocket had faced a pressure drop in one of the boosters, but the onboard computers aborted the rocket, barely two seconds before lift-off. ISRO top brass had then claimed that they had perfected the in-built safety systems to prevent a disaster.
On Monday it seemed like ISRO officials had a hint of a problem in the rocket, when they delayed the launch by almost one hour. But, they went ahead at 17:38 hours, to find television sets across the world beam the five-storeyed gigantic machine bursting into flames.
Post-Moterm:

But,The strap-on Boosters is belived to have developed a snag well before the launch, and according to some reliable sources, its actually the executive decession and the political will that made to go ahead with the launch even after the strapons developed some pressure loss., (meaning the motor used for pumping fuel din’t worked upto the mark.) (but the pride of completing the mission on the announced day seems to have rushed the decassion rather than wait for the saftey check to complete) all said and done, such accidents do happen and cannot be parted with, So i personally think the ISRO guys will come up with more robust and efficent “on-board ” security measures……

Knowledge needs to be free!
GSLV Failure, Yes this does happen., Now & then

GSLV Failure, Yes this does happen., Now & then

The Official Press Release from the ISRO is below and it describes that the GSLV “cannot complete its mission” ie. putting the satelitte on orbit. But, as it came to know the Liquid strap-ons were (seems to be ) the reason for this hitch too., (as was in 1999).

PRESS RELEASE
Date Released: Monday, July 10, 2006
Source: Indian Space Research Organisation
India’s Geosynchronous Satellite Launch Vehicle (GSLV-F02), with INSAT-4C on board, was launched from Satish Dhawan Space Centre SHAR (SDSC SHAR), Sriharihota today (July 10, 2006).

The lift-off took place at 5:38 p.m. IST.
However, GSLV-F02 could not complete the mission.

The detailed analysis of the data received from the vehicle is being analysed to pinpoint the exact reasons.

The Anatomy of the ” Failure “
The second operational flight of the GSLV rocket that was to hurl the country’s heaviest satellite yet built , 36,000 km into space instead plunged into the sea, within a minute of launch from the country’s space port at Sriharikota.
One of the four strap-on motors, attached to the 49-metre-tall, 414 tonne GSLV did not give the required thrust forcing the rocket to deviate from its flight path by about 10 degrees. The project director, who found that the first stage did not separate from the upper two stages, pressed the button to destroy the rocket for safety reasons. “It appears from preliminary data that the pressure had dropped to zero in one of the four strap-on motors and it failed to give the required thrust to the GSLV,” Indian Space Research Organisation (ISRO) Chairman G Madhavan Nair said, after the mishap, the first major incident in 12 launches of the space agency.(considering 9 Succesful launches in Row with 6 Foreign Satelittes/Payloads)
Five years ago, the first experimental GSLV rocket had faced a pressure drop in one of the boosters, but the onboard computers aborted the rocket, barely two seconds before lift-off. ISRO top brass had then claimed that they had perfected the in-built safety systems to prevent a disaster.
On Monday it seemed like ISRO officials had a hint of a problem in the rocket, when they delayed the launch by almost one hour. But, they went ahead at 17:38 hours, to find television sets across the world beam the five-storeyed gigantic machine bursting into flames.
Post-Moterm:

But,The strap-on Boosters is belived to have developed a snag well before the launch, and according to some reliable sources, its actually the executive decession and the political will that made to go ahead with the launch even after the strapons developed some pressure loss., (meaning the motor used for pumping fuel din’t worked upto the mark.) (but the pride of completing the mission on the announced day seems to have rushed the decassion rather than wait for the saftey check to complete) all said and done, such accidents do happen and cannot be parted with, So i personally think the ISRO guys will come up with more robust and efficent “on-board ” security measures……

Knowledge needs to be free!
Commercial Remote Sensing Satellite Market Stabilizing

Commercial Remote Sensing Satellite Market Stabilizing


Commercial Remote Sensing Satellite Market Stabilizing

Lately, trends have been leaning toward applications in urban planning and development and search-and-rescue operations. Comparative satellite imagery could also be used to track endangered species and to help protect the Earth’s natural resources.

In a new study, “The Market for Civil & Commercial Remote Sensing Satellites,” Forecast International is projecting deliveries of approximately 139 imaging satellites worth $16.3 billion over the next 10 years. The first half of the period will be more active than the second, with 97 spacecraft slated for production within the next five years.

Despite the ever-growing list of remote sensing spacecraft destined for orbit during the next 10 years, very few new players are expected to enter the commercial operator market.

The U.S. commercial remote sensing market is headed toward a period of stability thanks to the acquisition of Space Imaging by Orbimage, now known as GeoEye., without which there could be much chaos.

“The narrowing of the field from three down to two should take a burden off the U.S. government, as ensuring adequate support to all three U.S. players had been problematic,” said John Edwards, Forecast International Space Systems Editor.

“Leaning on this government support, U.S. remote sensing operators now seem content to court govern­ment business almost exclusively, as there is much less emphasis on development of the commercial base,” said Edwards. “A rebound toward the commercial side is anticipated but it’s not expected for at least another five years or more,” he added.

Through 2009 production lines will remain very active, turning out an average of 19 spacecraft per year. The overwhelming majority will be low-Earth-orbiting (LEO) satellites, with 19 such systems planned for 2006, followed by 23 in 2007 and 25 in 2008.

The value of annual LEO satellite production during the first half of the forecast period will range between $848 million at the low end and $3.2 billion at the high end. Production of the eight geostationary Earth-orbiting (GEO) spacecraft planned for the forecast period is valued at approximately $1.4 billion.

The top unit producer in the LEO remote sensing satellite market is expected to be the Indian Space Research Organization, which is forecast to supply 14 satellites over the next 10 years. “India’s production plans for remote sensing satellites are ambitious and unrivaled,” said Edwards.

“Of course, he added, “the United States has a handful of large satellites in the pipeline to serve individual companies like DigitalGlobe and GeoEye, but again, these serve individual companies, whereas the ISRO and Antrix drive the plans for Indian production.”

This centralized approach has led to one of the most powerful and cohesive satellite fleets in orbit. India currently owns and operates a fleet of six remote sensing satellites.

Over the next 10 years, as the shared aims for satellite-based imagery are realized, international cooperation on civil programs will become more mainstream. The markets for the data are myriad, starting with serving govern­ments during wartime, engineers during development, and farmers during the growing season.

Lately, trends have been leaning toward applications in urban planning and development and search-and-rescue operations. Comparative satellite imagery could also be used to track endangered species and to help protect the Earth’s natural resources.

Competition to sell these products is fierce, and Forecast International expects this competition to spur another round of limited consolidation during the forecast period.

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India Cancels Agni III Test

India Cancels Agni III Test

India Cancels Agni III Test


The Agni III (pictured) is said to be able to deliver a 440-pound to 550-pound warhead with a high degree of accuracy.



The Indian government has decided to cancel the first test-firing of its Agni III inter-continental ballistic missile.

The Agni III was the pride of the Indian strategic missile program and was designed to have a range of at least 1,400 miles, and possibly as far as 2,000 miles, giving it the capability of hitting cities across southern China with nuclear weapons.

According to a report in Asia Times Online May 25, U.S. pressure may have played a role in Prime Minister Manmohan Singh’s decision to cancel the test, which has angered pro-military hawks in the Indian defense establishment and right-wing Hindu nationalists.

“The United States has always been very suspicious about India’s Agni program, and in 1994 persuaded it to suspend testing of (earlier, shorter-range versions of) the missile after three test flights,” theAsia Times Online report said. The U.S.-backed Missile Technology Control Regime seeks to prevent the proliferation of missiles capable of delivering an 1,100-pound payload over distances of more than 180 miles.

“Decisions concerning the country’s strategic program, including the development and testing of different classes of missiles, are based on technical factors and a continuous review and assessment of our overall security environment,” an Indian Foreign Ministry spokesperson said.

The Agni III is said to be able to deliver a 440-pound to 550-pound warhead with a high degree of accuracy. The longest-range, surface-to-surface Agni III has reportedly been ready for launch for two years, but the tests have been repeatedly postponed, Asia Times Online said.

India’s military capabilities and arsenal are developed by the Defense Research and Development Organization which works in close coordination with space and nuclear-power institutions. “There is no doubt that it is the shadow of Washington and access to nuclear energy that finally tilted the scales against the Agni III.” the Asian Times Online report said

Indian Defence Minister Pranab Mukherjee has said that self-imposed “restraint” was behind India’s failure to test-fire the Agni III.

“Self-restraint does not mean that the DRDO (Defence Research and Development Organization) can’t go ahead with cold-bed tests for the missile’s subsystems,” he said.

However, Jane’s Defense Weekly noted on May 24 that Indian analysts have said Mukherjee’s “ambiguous” explanation was due to “sensitive and crucial” diplomatic and strategic talks with the United States and China. New Delhi did not want the Agni III to be a stumbling block during Mukherjee’s visit to Beijing this week. Missile tests could also hamper U.S. congressional ratification of the bilateral nuclear cooperation agreement offered by the United States, Jane’s Defense Weekly said.

An Agni III test launch would also send the “wrong signals” to the 45-member Nuclear Suppliers Group meeting in Rio de Janeiro in June, an Indian official told Jane’s.

However its understandable that the pro-nuclear hawks in the US is gunning for bush’s blood and specefically in this time when the crucial Indo-US civilian nuclear cooperation treaty is to be introduced in the senate, the reason behind the canceling of the test

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The Light Combat Aircraft : Tejas

The Light Combat Aircraft : Tejas

The Light Combat Aircraft : Tejas

LCA is the world’s smallest, light weight, multi-role supersonic combat aircraft. It has been designed to meet the requirements of Indian Air Force as its frontline multi-mission single-seat tactical aircraft.
It is India’s second indeginous fighter, the first one being the 1960’s HF-24(Hindustan Fighter) ‘Marut’. 129 Marut fighters were manufactured. Marut had limited supersonic capability (It could go supersonic in dives). The LCA will be the first supersonic combat aircraft to be built and flown in India itself. Interestingly, the requirements of both LCA and HF-24 and very similar. India had previously attempted to build a supersonic fighter : the HF-73, a development of the Marut. HF-73 was to use engines with more power. The project was cancelled after a crash.
LCA can be inducted starting 2008(as per a recent ADA Release) into the Indian Air Force (IAF) in limited numbers, though ‘full-scale’ induction won’t happen anytime before 2010. Further delays are expected. Most critics put the date of induction between 2012 and 2015.
The idea for this plane was born in 1983. It’s development has been an extremely painful process. The Indians had to develop most of the workings themselves, with some ‘hand holding’ by foreign firms. The US sanctions following their nuclear blasts only worsened the situation.
If the LCA succeeds, India may go ahead with development of the MCA, a stealthy twin-engined jet.

Development Plan
On 4th January 2001, India’s ‘Light Combat Aircraft’ or LCA flew for the first time. The maximum speed achieved was 400 kph and the maximum altitude was 3,000 m. The 18 min long test flight was performed by Wing Commander Rajiv Kothiyal. This plane was the LCA TD-1 and was given the serial number ‘KH2001’. ‘KH’ stands for Kota Harinarayana – Director of ADA while ‘TD’ stands for Technology Demonstrator. LCA TD-1 was powered by a General Electic F404-F2J3 turbofan.
No official name has been given to the LCA as yet, but it will probably get a HF-X designation. The word is ‘LCA’ is used in the same way ‘ATF’ is for F-22 Raptor.

Before the design is ready for induction, 5 Prototype Vehicles [PVs] will be constructed along with the 2 TDs. TD-1 and TD-2 are already flying. TD-2 flew after an agonising wait of 5 years after its roll-out in 1995. It completed its first block of 12 flights in June 2001 and was sent for modification before the next block of flights. TD-2 flew first on 6th June 2002. The 8th and 9th LCA prototypes built will be Naval version.
TD Vehicles, as the name itself suggest, are basically to prove the concept and test only the fundamental technology involved. PVs will be the final design, though minute changes should be possible still. LCA Prototype Vehicles will be lighter by an impressive 200 kg than TD-1. TD-2 itself was lighter than the TD-1. Work is under progress on the PVs. These are expected to be weaponised. PV-1 is expected to fly by the end of 2002. PV-5 will be a trainer and hence will be twin seat.
TD-2 specifically incorporates the following changes as compared to TD-1:
An indigenous Head Up Display (HUD) replaces the imported HUD. The new HUD, developed by CSIO, Chandigarh, has a larger field of view, three times the brightness, higher redundancy and is noiseless since the design does not call for a cooling fan.
An indigenous single LRU Integrated Communication System (INCOM) replaces a three LRU INCOM in LCA-TD1. The new INCOM developed by HAL , Hyderabad is a second generation software based system with significant weight saving (17 Kg), reduced volume(43% of original volume), and improved system performance and reliability.
A marginal reduction in empty weight of aircraft.
Longer flight duration with increased useable fuel.
Reduced noise levels in cockpit with improved ECS design. Cockpit noise was an unexpected problems initially encountered in TD-1.
Delays that have plagued the program since its inception, and they are expected to hinder plans even in the future.
If all goes well, LCA will go supersonic after atleast 100 hrs of flight testing. A minimum of 2000 flying hrs is needed to certify it ready for production. The first flight of TD-2 signalled the completion of the first 12 hrs. The development phase involving two technology demonstrators is estimated to have cost Rs. 21.88 billion.
Why India needs the LCA
The IAF heavily relies on the 1950’s design MiG-21 to maintain its numbers, if not its effective force. The LCA was essentially envisioned as a replacement for it. Delays in LCA’s development have caused a lot of problems – The MiGs are old, and unforgiving – pilots are losing their lives each year. Such is its reputation, that it is now called ‘the flying coffin’ in the pilot’s mess.
Part of the problem also arose from the fact that the IAF had to rely on the sub-sonic Kiran jet trainer for pilot’s training for last 15 years of the 20th Century. The junior pilots had to jump right from the Kiran to the bisonic MiG. IAF’s MiG-21Us are aeging too and limits the performance of these aircraft. It is not surprising that most deaths were those of young pilots. Only recently did the Government decide to acquire Hawk AJTs [Advanced Jet Trainer] from Britain. However, even after intense negotiations an agreement could not be worked out and acquisition of an AJT has been postponed to the unforseeable future.
During the decade 1990-2000 the IAF lost 172 MiG series aircraft in crashes, much more than its losses in wartime operations.During the two wars with Pakistan in 1965 and 1971 as well as the Kargil border conflict of 1999, the Indian Air Force lost a total of 115 aircraft. From 1995-2000 alone, the losses due to aircraft involved in accidents amounted to Rs 2.74 billion. During the same period, 52 pilots lost their lives in accidents. India has paid a very heavy price for LCA delays.
An $340 million upgrade program was started in 1996. These new aircraft are called MiG-21-93 in Russia and MiG-21UPG in India. While some will be upgraded in Russia, most upgradation will be done in India itself. The deal was meant to be completed within two years but the first two upgraded MiG-21-93 jets were only delivered to India in December 2000. The first 2 upgraded MiGs done in India were shipped to the IAF in May 2001. These new aircraft have a mix of French, Israeli, Indian and Russian equipment. It is claimed that the fighters are equivalent to any 4th Generation fighter, with the ability to lock on to 8 different targets at once. The upgrading of the 125 MiG-21s is now slated for 2005, with the implementation of the plan expected to enable the IAF to extend the life of the jets uptil 2015.
Apart from the MiG-21, LCA will also replace MiG-23 and MiG-27, also in service with the IAF.
Will the LCA itself be obsolete by 2015? Certainly not considering India’s main rivals, China and the Pakistan fly aircraft like the Chinese F-7(a copy of MiG-21). Other Chinese fighters include the FC-1 (Fighter China 1) and the J-10(F-10 for foreign markets).
Rivals

FC-1 is based on the MiG-33 which was rejected by the Soviet Air Force. MiG-33 was a single engined version of MiG-29. Pakistan hopes to buy 150 of them to replace most of its existing air force while the Chinese Air Force does not want to purchase it. Lastest reports say that FC-1 may never enter production – Russia has refused to supply the powerful RD-93 engine. Pakistan has given the FC-1 the ‘Super-7’ designation.
FC-1 has not been flown. Chengdu is working on it though, and models have been displayed at many exhibitions. While FC-1 design itself is not very advanced, the fact is that China will buy many avionics components from outside and hence has the capability of
getting the FC-1 into active service much before the LCA. However, recent reports suggest that it might now be replaced by a different design : J-7MF (a Chinese MiG-21 upgrade).

The J-10 started off as a chinese attempt at reverse engineering a Pakistan bought US F-16. However, it ended up being a modification of Israel’s Lavi (Young Lion) multirole fighter. Lavi program was cancelled in 1987 in Israel due to political reasons. A J-10 crash in 1995 forced a shift manufacturing plans till atleast 2005 (flights resumed in 1998). The J-10 is believed to be powered by 122.6kN (27,650 lb) Saturn AL-31F turbofans with afterburners.

Interestingly, both LCA and J-10 are due to serve on indigenous Indian and Chinese aircraft carriers, both set to sail by 2010.

Two other contemporary aircraft began in the same period (1982/83): the European Eurofighter Typhoon and Swedish Jas-39 Gripen. The eurofighter first flew in March 1994 while Gripen took off in December 1988. Gripen joined squadron in 1998(making it the first new 4th generation fighter of the world) while Eurofighter will in 2002. Both faced problems with their digital flight control systems which enable the inherently unstable delta-wing aircraft to fly by using computers to command its flight control surfaces and provide unusual moaneuverability to the jets. Both are being promoted in the foreign markets. JAS-39 has already been chosen by the South African Air Force as their backbone. It is infact regarded as a direct competition to the LCA.
Indians have boldly claimed that the “LCA has more advanced technology than JAS- 39 Gripen and as much advanced technology as the Typhoon.” And if it does, then it needs to be proved on the ground and in flight.
The Airplane
LCA has a double delta wing configuration with no tailplanes or foreplanes and features a single vertical fin. The LCA is constructed of aluminium-lithium alloys, carbon-fibre composites, and titanium. It’s design has been configured to match the demands of modern combat scenario such as speed, acceleration, maneuverability and agility. Other features of the design include Short takeoff and landing, excellent flight performance, safety, damage-tolerant design, reliability and maintainability.
According to current estimates, the LCA will cost about $17-$20 million and efforts are being made to bring down the cost to $15 million. At this price the LCA has considerable bang for buck value. In comparison, a Su-30 fetches $35 million per piece for Russia, while France’s Rafale cost $70+ million.
It integrates modern design concepts and the state-of-art technologies such as relaxed static stability, flyby-wire Flight Control System, Advanced Digital Cockpit, Multi-Mode Radar, Integrated Digital Avionics System and a Flat Rated Engine.
Around 70% of the jet is to be made in India itself. The rest will have to be imported for sometime. No mistake must be made with regards to LCA’s modernity and design. It is truly advanced and has all the necessary equipment and more.
A naval carrier based version of LCA is also being developed. This version will feature a strengthened undercarriage and sturucture, additional leading edge control surfaces (in the area where the wing joins the fuselage) and lowered nose for better visibility. News reports suggest that US help has been sought for the LCA Navy. The 8th and 9th LCA prototypes built will be Naval version.

Air Frame Among the most significant breakthrough is the use of advance carbon composites for more than 40% of the LCA air frame, including wings, fin and fuselage. Apart from making it much lighter, there are less joints or rivets making the aeroplane more reliable. Fatigue strength studies on computer models optimise performance. National Aerospace Laboratory (NAL) has played a lead role. Materials include Aluminium – Lithium alloys , Titanium alloy and Carbon compositites. Composities for wing (skin , spars and ribs ) fuselage (doors and skins), elevons, fin, rudder, airbrakes and landing gear doors.
The skin of the LCA measures 3 mm at its thickest with the average thickness varying between 2.4 to 2.7 mm. BAe was consulted. The fin for the LCA is a monolithic honeycomb piece. No other manufacturer is known to have made fins out of a single piece. The cost of manufacture reduces by 80 per cent from Rs 2.5 million in this process. This is contrary to a subtractive or deductive method normally adopted in advanced countries, when the shaft is carved out of a block of titanium alloy by a computerized numerically controlled machine. A ‘nose’ for the rudder is added by ‘squeeze’ riveting.

A striking feature of the LCA is its small size. It is much smaller than even the JAS-39, which a ~1m longer. An effort was made to reduce the number of individual composite parts to the minimum and hence keep the plane light.
The use of composites results in a 40 per cent reduction in the total number of parts (if the LCA were built using a metallic frame): For instance, 3,000 parts in a metallic design would come down to 1,800 parts in a composite design. The number of fasteners has been reduced to half in the composite structure from 10,000 in the metallic frame. The composite design helped to avoid about 2,000 holes being drilled into the airframe. Though the weight comes down by 21 per cent, the most interesting prediction is the time it will take to assemble the LCA — the airframe that takes 11 months to build can be done in seven months using composites.
When lightning strikes the LCA, four metal longerons stretching from end to end, afford protection. In addition, all the panels are provided with copper mesh. One out of five is ‘bonding’ bolt with gaskets to handle Electr-Magnetic Interference. Aluminum foils cover bolt heads while the fuel tank is taken care of with isolation and grounding.
LCA is expected to be highly maneuverable by virtue of its double delta wing and relaxed static unstability of its Fly-By-Wire system.
Flight Control and Software and Other Avionics
The LCA uses advanced digital fly-by-wire technology which essentially employs computers to optimise the aircraft’s performance. Foreign companies were consulted. Infact, LCA avionics were first flight tested on a US F-16XL.

Witout the automatic flight control, the LCA will not be flyable, due to the Delta wing’s inherent instability. As more and more flights are conducted, the software is updated to allow the aircraft to do more complex maneuvours. To combat the threat of obsolescence in the LCA Programme, a concerted effort has been made to introduce an Open-architecture Avionics system which permits hardware scalability and upgradability to state-of-the-art technology levels with reusability of the software.
LCA Avionics architecture is configured around a three bus system (MIL-STD-1553B) in a distributed environment. The heart of the system is a 32-bit Mission Computer (MC) which performs mission oriented computations, flight management, reconfiguration / redundancy management and in-flight system self-tests. In compliance with MIL-STD-1521 and 2167A standards, Ada language has been adopted for mission computer software.Accurate navigation and guidance is realised through RLG based Inertial Navigation System (INS) with provision for INS / Global Positioning System (GPS) integration. Jam resi
stant radio commumication system with advanced Electronic Warfare (EW) environment. In the EW suite, Electromagnetic and Electroptic receivers and jammers provide the necessary “soft-kill” capability.
The digital FBW system of the LCA is built around a quadruplex redundant architecture to give it a fail op-fail op-fail safe capability. It employs a powerful Digital Flight Control Computer (DFCC) comprising four computing channels, each powered by an independent power supply and all housed in a single line replaceable unit (LRU). The system is designed to meet a probability of loss of control of better than 1×10-7 per flight hour. The DFCC channels are built around 32-bit microprocessors and use a safe subset of Ada language for the implementation of software. The DFCC receives signals from quad rate, acceleration sensors, pilot control stick, rudder pedal, triplex air data system, dual air flow angle sensors, etc. The DFCC channels excite and control the elevon, rudder and leading edge slat hydraulic actuators. The computer interfaces with pilot display elements like multifunction displays through MIL-STD-1553B avionics bus and RS 422 serial link.
For maintenance the aircraft has more than five hundred Line Replaceable Units (LRUs), each tested for performance and capability to meet the severe operational conditions to be encountered.
Mission Computer(MC): MC performs the central processing functions apart from performing as Bus Controller and is the central core of the Avionics system. The hardware architecture is based on a dual 80386 based computer with dual port RAM for interprocessor communication. There are three dual redundant communication channels meeting with MIL-STD-1553B data bus specifications. The hardware unit development was done by ASIEO, Bangalore and Software Design & Development by ADA.
Control & Coding Unit (CCU): In the normal mode, CCU provides real time I/O access which are essentially pilot’s controls and power on controls for certain equipment. In the reversionary mode, when MC fails, CCU performs the central processing functions of MC. The CCU also generates voice warning signals. The main processor is Intel 80386 microprocessor. The hardware is developed by RCI, Hyderabad and software by ADA.
Display Processors (DP): DP is one of the mission critical software intensive LRUs of LCA. The DP drives two types of display surfaces viz. a monochrome Head Up display (HUD) and two colour multifunction displays (MFDs). The equipment is based on four Intel 80960 microprocessors. There are two DPs provided (one normal and one backup) in LCA. These units are developed by ADE, Bangalore
Mission Preparation & Data Retrieval Unit (MPRU): MPRU is a data entry and retrieval unit of LCA Avionics architecture. The unit performs mission preparation and data retrieval functions. In the preparation mode, it transfers mission data prepared on Data Preparation Cartridge (DPC) with the help of ground compliment, to various Avionics equipment. In the second function, the MPRU receives data from various equipment during the Operational Flight Program (OFP) and stores data on Resident Cartridge Card (RCC). This unit is developed by LRDE, Bangalore.
USMS Electronic Units:
The following processor based digital Electronics Units (EU) are used for control and monitoring, data logging for fault diagnosis and maintenance.
Environment Control System Controller (ECSC)
Engine and Electrical Monitoring System Electronics Unit (EEMS-EU)
Digital Fuel Monitoring System Electronics Unit (DFM-EU)
Digital Hydraulics and Brake Management System Electronics Unit (DH-EU)
V/UHF Equipment: V/UHF equipment is a secure jam resisant airborne radio communication set which provides simplex two way voice and data communication in the VHF and UHF frequency bands. This unit is developed by HAL, Hyderabad.
Multi Function Keyboard (MFK):
MFK is an interfce for pilot dialogue concerning certain selected equipment of Avionics system. It comprises LCD panel, alphanumeric keys, push buttions for power ON / OFF and LEDs indicating power ON / OFF status of certain Avionics equipment. This unit is developed by BEL, Bangalore.
Head Up Display (HUD): HUD is of conventional type with a Total Field of View (TFOV) of 24 degrees circular. A Change Coupled Device (CCD) based camera is mounted on the HUD for recording purposes. HUD dsplays various navigation and weapon related data. This unit is developed by CSIO, Chandigarh.
Colour Multi Function Displays (MFDs): LCD based colour MFDs hava a useful screen area of 125 mm x 125 mm. They have soft keys around their periphery for interaction with the systems. This display provides various aircraft system pages and navigation pages in addition to RADAR & FLIR display.
Digital fly-by-wire Flight Control System is another advanced feature of LCA. The unstable configuration of LCA demands a highly efficient Integrated Flight Control System (IFCS) to fly the aircraft. Control law resident in the flight control computer synthesises inputs from pilot’s stick and rudder pedals with flight parameters from inertial and airdata measurements to generate commands to the actuators that move various control surfaces. The design of the control law is evaluated susing real-time flight simulator for acceptable flight handling qualities. The IFCS ensures stability, agility, manoeuvrability and carefree handling over the entire operating envelope of LCA. The Digital Flight Control Computer (DFCC) is the heart of IFCS, and uses a quadruplex redundant system to achieve high reliability and safety.
Independent Verification and Validation (IV&V) activity is an integral part of the Software development process. From requirement specification to final testing, IV&V ensures correctness, consistency, completeness and adherence to MIL standards of the software.
The flight control system along with all the associated software is tested and validated at the iron-bird rig.
The Cockpit
Its new-generation glass cockpit has the latest avionics systems for pilot comfort and efficiency. No tangle of dials and switches. Multi-function digital displays provide information of all vital parameters with the click of a button. Critical information is flashed on the head-up display. Aeronautical Development Establishment (ADE) and NAL were major partner in these developments.

Two Multi Function Displays present required information to the pilot. Critical information required in close combat situations is flashed onto the Head Up Display. Hands on Throttle and Stick (HOTAS) concept ensures availability of every control needed during a critical combat situation, right under the fingers of the pilot. The Environmental Control System (ECS) is designed to give a high degree of comfort to the pilot and to provide adequate cooling to all onboard electronic systems. The compressed air for pressurisation of cockpit, radar and fuel tank is also supplied by ECS.
ADA has also tied up with India’s National Institute of Design (NID), Ahemdabad to bring in the elements of ergonomics and modular design. The aim is to help build the aircraft in such a manner that it has more standardised units or dimensions allowing increased flexibility. The NID design team for this project will be lead by Dr S Ghosal who is the director of NID’s Bangalore centre.
Weapons
The LCA has a choice of seven pylons three under each wing and one under its fuselage to c
arry a wide range of armoury. It is designed to be a precision launch platform with air-to-air missiles and air-to-ground weapons, including laser guided bombs. A total of 4000 kg can be carried. Plenty of work to be done. It is expected that the R-73 (AA-12 Archer) will be integrated into the PV-1.
LCA will be armed with a Gasha Gsh-23mm gun. The R-73 will be directed by a Helmet Mounted Sight (HMS) ensuring quick action. It is not clear what medium range AAMs it will carry – the IAF currently operates the Matra Super 530D, R-27RE1 and RVV-AE(R-77) BVR missiles. The choice depends a lot on the radar, unlike dogfight missiles which are usually heat seeking. For example, IAF has integrated both Magic-2 and R-60MK with the MiG-21. A range of weapons, from Russia, West or India will be made available.
A total of 7 hardpoints will be available: 3 on each wing plus one under the fuselage.
As the name itself suggests, LCA’s delivery capacity will not be high compared to say the Su-30, but it can carry as much as the MiG-2ML, which the IAF’s primary Close Air Support (CAS) fighter. Hence even with LCA’s multi-role capability the IAF will need a ‘bigger’ fighter – the Su-30MKI Super Flanker has already been picked as its frontline fighter for the first Quater of the 21st Century (Su-30MKI Info and pictures).
RadarThe multi-mode radar is to take care of detection, tracking, terrain mapping and delivery of guided weapons. The track-while-scan feature keeps track of multiple targets (maximum 10) and also allows simultaneous multiple target engagement. Pulse-Doppler gives the look-down shoot-down capability. Ground mapping feature, frequency agility and other ECCM techniques make the radar truly state-of-the-art.
The antenna is a light weight (less than 5 kg), low profile slotted waveguide array with a multilayer feed network for broad band operation. The salient technical features are: two plane monopulse signals, low side lobe levels and integrated IFF, and GUARD and BITE channels. The heart of MMR is the signal processor, which is built around VLSI-ASICs and i960 processors to meet the functional needs of MMR in different modes of its operation. Its role is to process the radar receiver output, detect and locate targets, create ground map, and provide contour map when selected. Post-detection processor resolves range and Doppler ambiguities and forms plots for subsequent data processor. The special feature of signal processor is its real-time configurability to adapt to requirements depending on selected mode of operation.
To be jointly developed by State owned HAL and Electronics Radar Development Establishment (ERDE) the project has run into major delays and cost escalations.
Two Avro aircraft – HS748M have been modified for the purposes of testing the radar. The idea of doing these tests on an Avro is that these planes can fly for a longer time and hence collect a lot more data.
PV-2 is planned to be equipped with the Radar and Fire Control System (FCS).
Engine & Fuel System
Kaveri engine is a two-spool bypass turbofan engine having three stages of transonic low pressure compressor driven by a single-stage low pressure turbine. The core engine consists of six-stage transonic compressor driven by single-stage cooled high pressure turbine. The engine is provided with a compact annular combustor with airblast atomisers. The aerothermodynamic and mechanical designs of engine components have been evolved using many in-house and commercially developed software for solid and fluid mechanics.

Kaveri three-stage transonic fan, designed for good stall margin and bird strike capability, handles an air mass flow of 78 kg/s and develops a pressure Combustion Chamber Liner ratio of 3.4. The six-stage variable capacity transonic compressor of Kaveri develops a pressure ratio of 6.4. The variable schedule of inlet guide vanes and two rows of stator is through FADEC control system to open the stator blades in a predetermined manner. High intensity low UD ratio annular combustor of Kaveri engine incorporates air blast injection of fuel for uniform outlet temperature profile and reduced carbon emission.
Kaveri high pressure turbine is provided with an efficient cooling design incorporating augmented convection-cum-film cooling for the vanes and combination cooling for the rotor blade to handle up to 1700 K turbine entry temperature. Kabini engine comprising high pressure compressor, combustor and high pressure turbine has undergone high altitude test at facilities abroad successfully demonstrating the flat rating concept of Kaveri engine assembly and in particular the combustor high altitude ignition and stability performances.
Kaveri engine has been specifically designed for Indian environment. The engine is a variable cycle-flat-rated engine in which the thrust drop due to high ambient, forward speed is well compensated by the increased turbine entry temperature at the spool Kabini altitude test speed. This concept has been already demonstrated with high temperature and pressure condition in DRDO’s High Mach Facility. Kaveri engine is controlled by Kaveri full authority digital control unit {KADECU), which has been developed and successfully demonstrated at DRDO’s test bed.
Kaveri
Air-mass flow
78 kg/s
By-pass ratio
0.16
Overall pressure ratio
21.5
Turbine entry temperature
1487-1700 K
Maximum dry thrust
52 kN (5302 kg)
Maximum dry SFC
0.78 kg/hr/kg
After burner maximum power thrust
81 kN (8260 kg)
After burner maximum power SFC
2.03 kg/hr/kg
Thrust-to-weight ratio
7.8
Currently, the protoypes are powered by the US made GE F404 engine. India’s Defence Research and Development Organisation [DRDO] had purchased 11 F404 engines for the LCA project in the 1990s but further collaboration with the engine’s manufacturers is no longer possible due to sanctions imposed by the US in the wake of India’s nuclear tests of 1998. The US sanctions against India have now been lifted by the Bush Administration. Another lot of 40 engines were ordered but it is not clear whether the deal has been signed on the dotted line.
The HF-24 Marut could not achieve its full potential due to the abscence of a suitable powerplant. Currently, the only Jet Engine developed completely in India remains the one used in the Lakshya drone.
The State owned Gas Turbine Research Establishment [GTRE] was to indigenously develop the Kaveri engine to power the LCA. But there have been major slippages in all the milestones apart from cost overruns of Rs 380 crore. It is difficult work but is finally getting underway.
It was initially expected that a LCA (PV-1) with a Kaveri engine will fly in 2002 – it now seems unlikely it will. GRTE has made four Kaveri engines and one of these, the K4, will be sent to Russia [which has inexpensive testing facilities] for high-altitude tests in the second half of 2001. The test-bed is a Tupolew Tu-16 bomber. These airborne tests will allow Indian scientists to study the functioning of the engine in flight. Some 80 hrs of airborne testing and around 1000 hrs of ground testing had been completed by February 2001. Atleast 1000 hrs of flight testing are needed for air-worthiness certification.
The Jet Fuel Starter [JFS] GTSU-110 is indigenous and has the capability to provide in flight starting of the LCA main engine up to an altitude of 6 km. It has been successfully tested at Leh, which has the world’s highest altitude airport.
It
is now clear that the LCA will be inducted initially with GE engines and later be upgraded with the Kaveri. It is now certain that atleast the first couple of PVs will be powered by the F404.
Fuel tanks are integrated into the fuselage and wings. For extended range, additional 800 lt / 1200 lt fuel tanks are carried at midboard / inboard wing stations and also at centreline station under the fuselage. The inflight refuelling probe further extends the range and endurance.
The GE F404 is a rather popular engine: F/A-18 Hornet, F-117 Nighthawk and even the famed B-2 Stealth bomber is powered by (Four) F404s! The JAS-39 too is powered by a modification of the F404 made by Volvo. When the Rafale prototype first flew, it too had the GE F404 engines. The Rafale has entered service with the M88 and infact the M88 has been offered to India. Now that the sanctions are gone, it is unlikely that either the M88 or the other european counterpart EJ200 (used in the Eurofighter and perhaps later in the JAS-39) will ever be seen in the LCA. Snecma however, is collaborating with GTRE to develop the Kaveri.
Stealth Features
Stealth is an important feature for all new combat aircraft coming up. LCA does not have any stealth charactristics like in F-117 or F-22, but considering its small size, tail-less design and simple delta wing config, a GE-404 engine(atleast for now) – which is also used in the F-117 – it should be stealthier that atleast a MiG-21 or MiG-23/27. It is also expected that LCA will get DRDO developed Radar-absorbent paint. Composites are inherently stealthier than metal.
Timeline
Note: Rs 1 crore = Rs 10 million, $1 = Rs 47
1985: LCA launched with a time frame of 10 years after the Union cabinet sanctioned Rs 560 crore for the project in 1983. Aeronautical Development Agency to be the nodal agency.
1988: ADA prepares project definition phase (PDP) after consulting MBB, France, on some aspects.
1990: Air HQ finds PDP deficient in crucial parameters. Expert committee formed to resolve deadlock. It is agreed that two technology demonstration aircraft to be built before investments cleared for production.
1993: After three years of uncertainty, Phase 1 is sanctioned at a cost Rs 2,188 crore. Milestones include a roll out of first aircraft by 1995 and first flight by 1996.
1995: Roll out does happen but there are serious doubts as to whether the first flight would occur as major problems bedevil flight control systems as well as mastery over composites.
1998: With the aircraft far from ready, the US sanctions after Pokhran tests cause setbacks in flight control technologies and systems integration.
1999: Low speed and high speed taxi trials are done. But flight trials delayed because of minor fire caused by overheating valve near cockpit.
2001: First flight on January 4. More flights follow, including one on Feb 9 at Aero India 2001 [Bangalore, February 7 to 11]. It completes it’s first block of tests on June 2.
Within 10 days after the first flight, both MiG and Sukhoi Bureaus expressed desire for joint LCA manufacture. Deputy Prime Minister[Russia] Ilya Klebanov too brought up this issue during his visit to India. They also offered to co-operate with India to develop a 5th Generation fighter(LFI). Other 5th gen aircraft include USA’s ATF F-22 Raptor and Joint Strike Fighter [JSF].
LCA completed its first batch of tests in 12 flights instead of 15 – ahead of schedule – on June 2, 2001. TD-1 was subsequently sent for further modifications including advanced flight controls software as well as extended range of flight endurance.
For TD-1’s block of first 12 flights:
Max Velocity: 610 km/h(0.71 Mach) Max Altitude: 8 km Max Angle of Attack: 18 degrees
Aeronautical Development Agency (ADA) and Hindustan Aeronautics Limited (HAL) signed a Memorandum of Understanding (MOU) for Limited Series Production of Indian LCA. 8 aircraft are to be delivered by 2006.

2002: The TD-2 (KH2002) flies for 30 mins on 6.jun.2002. It is piloted by Wing Commander Tarun Banerjee.
India now has 4 pilots who have flown the LCA. Wing Commander Kothiyal flew the first six on TD-1, Wg. Cdr. Nambiar piloted the TD-1 on the next six flights. Wg. Cdr. Banerjee flew the TD-2 on its first 4 flights. “I think it’s going to be an aircraft that our fighter pilots are going to love”, he remarked after the first one. Sqd Ldr Sunith Krishna flew for the first time in the LCA on the TD-2’s 5th flight.
Following TD-2’s first flight, Kota Harinarayan left ADA for a stint at the Indian Institute of Science (IISc), Bangalore. M.B.Verma took over as Programme Director.
Along with the LCA, India is also developing aircraft like Saras, a 14 seater civilian turboprop aeroplane, Hansa trainer and Intermediate Jet Trainer [IJT]. The sub-sonic IJT, whose first flight should take place in 2002, will replace the aged Kiran jet trainers. IJT shares some 100 parts with the LCA. The IAF has placed orders for 225 such aircraft which cost $5 million a piece.
TD-2 during its first flight (Right). TD-2 raised its undercarriage on this flight unlike the TD-1.These are vidcaps from the Mirage-2000TH chase plane that is employed on every LCA flight.
Total number of LCA TD-1 (KH2001) flights (Last Flight June 2, 2001) : 12
Total number of LCA TD-2 (KH2002) flights (Last Flight August 17, 2002) : 5
Stats
Length :
13.2 m
Height :
4.4 m
Wingspan :
8.2 m
Weight :
5.5 ton
Max. Speed :
Mach 1.8
Propulsion :
GE-F404 F2J3 18,097 lbs GTRE GTX-35VS Kaveri 20,200 lbs
Armament :
7 stations, 4 ton
Altitude :
50,000 ft
Fuel capacity:
3000 L
Flight Record
TD-1 (KH2001)
1.
January 4, 2001
18 min3100 m(wheels down)
2.
January 30, 2001
52 min
3.
February 3, 2001
23 min
4.
February 9, 2001(Aero India 2001)
~20 min4000 m560 kmph
5.
2001

6.
2001

7.
March 20, 2001

8.
2001

9.
2001

10.
2001

11.
May 31, 2001

12.
June 2, 2001

TD-2 (KH2002)
1.
June 6, 2002
28 min600 kmph
2.
July 6, 2002
30 min
3.
July 9, 2002
30 min
4.
July 26, 2002
~60 min(?)
5.
August 17, 2002
26 minPilot: Sqdn Ldr Sunith Krishna
The development effort for the LCA is lead by ADA. Apart from govt labs and agencies, many educational institutes and private companies also have a role. A list of some of the government agencies involved in the LCA and MCA projects:
Aeronautical Development Agency (ADA)
Aeronautical Defense Establishment (ADE)
Defense Research and Development Organisation (DRDO)
Hindustan Aeronautics Limited (HAL)
National Aerospace Laboratries (NAL)
Gas Turbine Research Establishment (GTRE)
National Test Flight Centre (NTFC), Hosur (near Bangalore)
Electronic Radar Development Establishment (ERDE)
Council for scientific and Industrial Researh(CSIR)
Some of the people associated with LCA development:
ADA Programme Director: M.B.Verma
Programme Director,NFTC: Air Marshal Philip Rajkumar
Project Director,General Systems: K.G. Vivek
K.V.L.Rao, Project Director,Propulsion Systems
T.G.Pai, Project Director,Technology Development, LCA Navy
M.B.Verma, Project Director, General System
Director-General, Aeronautical Development Agency (ADA): Vasudeva Aatre
Test/Chase Pilots: Wing Commander Rajiv Kothiyal, Wing Commander R Nambiar, Wing Commander Banerjee
Director, National Institute of Advanced Studies: Roddam Narasimha(chairman of the committee that reviewed the LCA in 1990)
HAL Chairman: C.G. Krishnadas Nair
NID LCA Team Leader: Dr S Ghosal
Head of Advanced Composites Unit,NAL: M.Subba Rao
Director-General (CSIR): Dr R.A Mashelkar

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Manned Spaceflight Plans For India To The ISS And Beyond

Manned Spaceflight Plans For India To The ISS And Beyond

Manned Spaceflight Plans For India To The ISS And Beyond

The Geostationary Launch Vehicle that ISRO has already successfully used three times can put at least two or three tons into low Earth orbit (LEO). From its launch site on the Bay of Bengal, it could reach the ISS with a reasonable load of fuel, water, or other supplies. This India Space Logistics Vehicle (ISLV) could be designed by India’s own space industry, with minimal help from the US or Russia, and prove to be far more cost effective than existing craft. Mumbai, India (SPX) Jan 16, 2006India is at a crossroads in its national space development program, having to decide if it will invest more of its small budget on manned space flight – which could be very lucrative, long-term, but which depends on certain conditions beyond its present control- or on continued robotic and scientific missions designed to benefit national development goals.Indian Space Research Organisation’s Chairman, G Madhavan Nair, recently announced that his country will decide in a year’s time on whether to develop a manned space mission.
“We have to first decide how far such a manned mission is beneficial and whether we can afford to remain without it. Only a national debate can throw up answers for a consensus to go for a manned mission,” he said. Such a program is expected to cost up to Rs 15,000 to 20,000 crore.
“We need to develop a lot of new technologies to build a life-supporting system, a space capsule with safety features to survive, and a recovery operation to complete the mission. If it is decided, then we do not want to lag behind in our preparations,” Nair said, adding it will take at least seven to eight years for the agency to prepare for the mission.
An un-manned mission, by comparison, would cost around Rs 3000 crore, “therefore, it has to be debated and decided whether it is worthwhile to go on with a manned mission, when the same can be achieved by robotic instruments,” he added.
India sent its first astronaut, Rakesh Sharma (the 138th astronaut to go into space), aboard the Soviet spacecraft Salyut 7 in April 1984, while another astronaut, the Indian-American Kalpana Chawla (who flew into space on board the Challenger twice), was killed along with six others in the Columbia shuttle disaster in February on February 1, 2003.
The United States offered to include an Indian astronaut in future manned-space missions during Prime Minister Manmohan Singh’s visit to Washington, in July 2005, but haven’t made any further commitments yet.
“ISRO is still reviewing the possibility of sending an Indian astronaut in the US-backed International Space Mission. But so far no such proposal has been drafted”, Mr Nair also said recently.
If an Indian citizen were to visit the ISS, alleged areas of study would include protein synthesis, aerobic cell cultivation and efficacy of yogic exercises under micro gravity.
Since the Soviets orbited Rakesh Sharma in 1984, India has refocussed its space activities on finding ways to use space technology for the direct benefit of India’s national development goals. As India becomes a greater player in the global economy, though, ISRO’s policy is changing – with the Chandrayaan 1 moon probe a sign, perhaps, that India is aiming at becoming a full-fledged space power with civilian, commercial, military, and even human space capabilities.
The key to helping India build its human spaceflight program is the United States’ role in the ISS partnership. As an apparent new long-term strategic and economic partner of the US, it’s in America’s national interest to see India develop some of its space activities in close cooperation with the US.
President Bush has committed the US to finishing the ISS assembly process by around 2010, which it will then use for human spaceflight research, until about 2015, after which, it plans to stop funding ISS operations and concentrate on the human exploration of the Moon and Mars.
There are no official US plans for the ISS after this date but it seems unlikely that America’s partners would abandon the complex. It is probable that, within the next few years, negotiations will begin covering the long-term future of the ISS, whereby the US might consider handing over to India some of its ownership rights in the ISS. If this happens, one could expect future ISS crews to include at least one Indian astronaut.
After 2015 the ISS partnership will have to evolve into something quite different from what it is today. The US will fade into the background while the Russians, Japanese and Europeans will share the leading roles. India – and perhaps China – will have the chance to fill the void left by the Americans.
India would earn its stake in the ISS by developing and building an automated logistics spacecraft, like Russia’s Progress or Europe’s Automated Transfer Vehicle (ATV).
The Geostationary Launch Vehicle (GSLV) that ISRO has already successfully used three times can put at least two or three tons into low Earth orbit (LEO). From its launch site on the Bay of Bengal, it could reach the ISS with a reasonable load of fuel, water, or other supplies. This India Space Logistics Vehicle (ISLV) could be designed by India’s own space industry, with minimal help from the US or Russia, and prove to be far more cost effective than existing craft.
India may even want to design the ISLV so that it could evolve to deliver cargo anywhere within cislunar space, including, eventually, the surface of the Moon. A low-cost, Earth-to-Moon supply carrier, launched by a future version of the GSLV, might be a valuable business niche for India’s future, giving the country a strong claim for participation in the Vision for Space Exploration.

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