Screambowl
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Possible test flight in Mid 2012.
so space shuttle is no time soon .
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Possible test flight in Mid 2012.
so space shuttle is no time soon .
Cryogenic Engine Failure Analysis
On Sunday, April 18, 2010, after a two day meeting chaired by ISRO Chief K. Radhakrishnan to analysze GSLV D-3 telemetry data, space scientists announced that the CUS ignited but shut down within a second because the turbo pump supplying fuel to the engine stopped working.
"The data clearly shows that combustion [of the cryogenic engine fuel, liquid hydrogen at minus 253 degree Celsius, and the oxidiser, liquid oxygen at minus 183 degree Celsius] had indeed taken place. The rocket's acceleration had increased for a second before it drifted off the designated flight path. Indications are that the turbine that powered the fuel turbo pump had somehow failed. [The propellants are pumped using turbo pumps running around 4,000 rpm.] There could be various reasons for its failure," a senior ISRO scientist told The Hindu.
A 'Failure Analysis Committee' will now attempt to zero in on the exact reason for the failure and submit its report by May-end. Next, the national experts' panel, constituted to review and give clearance to the GSLV-D3 mission, will examine the report.
Failure Analysis Committee Pinpoints Cause of Failure
The committee submitted its report on July 9, 2010. It attributed the failure of the third stage to a malfunction of the Fuel Booster Turbo Pump in the liquid hydrogen tank of the CUS.
The following are relevant excerpts from the committees report:
"Following a smooth countdown, the lift-off took place at 1627 hrs (IST) as planned. All four liquid strap-on stages (L40), solid core stage (S139), liquid second stage (GS2) functioned normally.
The vehicle performance was normal up to the burn-out of GS-2, that is, 293 seconds from lift-off. Altitude, velocity, flight path angle and acceleration profile closely followed the pre-flight predictions. All onboard real time decision-based events were as expected and as per pre-flight simulations.
The navigation, guidance and control systems using indigenous onboard computer Vikram 1601 as well as the advanced telemetry system functioned flawlessly. The composite payload fairing of 4 metre diameter inducted first time in this flight, also performed as expected. Performance of all other systems like engine gimbal control systems and stage auxiliary systems was normal.
The initial conditions required for the start of the indigenous Cryogenic Upper Stage (CUS) were attained as expected and the CUS start sequence got initiated as planned at 294.06 seconds from lift-off.
Ignition of the CUS Main Engine and two Steering Engines have been confirmed as normal, as observed from the vehicle acceleration and different parameters of CUS measured during the flight. Vehicle acceleration was comparable with that of earlier GSLV flights up to 2.2 seconds from start of CUS. However, the thrust build up did not progress as expected due to non-availability of liquid hydrogen (LH2) supply to the thrust chamber of the Main Engine.
The above failure is attributed to the anomalous stopping of Fuel Booster Turbo Pump (FBTP). The start-up of FBTP was normal. It reached a maximum speed of 34,800 rpm and continued to function as predicted after the start of CUS. However, the speed of FBTP started dipping after 0.9 seconds and it stopped within the next 0.6 seconds.
Two plausible scenarios have been identified for the failure of FBTP, namely, (a) gripping at one of the seal location and seizure of rotor and (b) rupture of turbine caused probably due to excessive pressure rise and thermal stresses. A series of confirmatory ground tests are planned.
After incorporating necessary corrective measures, the flight testing of Indigenous Cryogenic Upper Stage on GSLV is targeted within a year."
In the meantime, the next two GSLVs would fly with the available Russian Cryogenic Stages.
Indian Cryogenic Engine Second Test Flight
ISRO's CUS will be tested for the second time on GLSV D-5 in the middle of 2012. The launcher will be carrying GSAT-14.
Cryogenic Engine Test Facility
ISRO has built a new facility for static testing of the cryogenic engine at the Liquid Propulsions Systems centre (LPSC) at Mahendragiri.
Speaking to the press on June 18, 2011, after inaugurating a two-day National Conference on "Expanding Frontiers in Propulsion Technology," ISRO Chairman K Radhakrishnan said the facility will be ready in another two months an will be a big boon for the LPSC.
More Powerful Cryogenic Engine
ISRO is already working on a more powerful version of the cryogenic engine that it has developed.
"Our next step is to develop a bigger cryogenic engine with a stress of 20 tons compared to 7.5 tons now," ISRO Chairman, G Madhavan Nair, told PTI in September 2009.
The current version of the Indigenous Cryogenic Engine develops a thrust of 73 kilo Newtons (kN) in vacuum with a specific impulse of 454 seconds and provides a payload capability of 2200 Kg to Geosynchronous Transfer Orbit (GTO) for GSLV.
Work is underway to increase the thrust to 90 kN.
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Shuttle is a whole different ball game . They need to test it on earth first and then unmanned tests in space. But yeah, we would have the base rocket to launch one.
jha
Sir jee, where did i say that India should remain agri. based economy.. But the truth is (however bitter it may be ) that more than half of our population is engaged in this.. Whose responsibility is to provide them an alternative..?
Your original statement was so unfortunate that i had decided not to reply..
BTW Information itself is not enough.. Huge fund is required to teach them and provide them the necessary tools..
As i said before, that's not possible.. I can never be anti India..Its just my way of thinking does not suite you.
You are talking about AVATAR..I dont know if the program is still ON..
They are talking about Avatar, the report says unmanned space plane. It's the media that's comparing it with the Space shuttle and the Buran.
It's not the Avtaar. Who told you that the Avtaar was unmanned? This RLV is unmanned during tests so they can test for safety. They will not man the vehicle till they achieve all safety parameters for takeoff and touchdown landing.
Bhai saab.. The lack of fund is a major contributor (atleast for my Bihar )....Fund was not made available to us for building power projects.. There is no infrastructure and yet no special fund is given to us..
Not at all..People who are rich are entitled to be so..But this ever expanding gap between rich and poor has to reduce..
And lambasting the effort of Poor is a rather unfortunate comment.. No one wants to be in a mess where he has to kill himself and his family..
The concept looks alien to us (the "Rich ..?") but its true..India can not become a capitalist country.. We are a social welfare state with socialism at its core..
Here comes another pseudo socialist. That bloody socialism has left us in tatters that we are in today. Don't mind me saying this but world doesn't work on social welfare but on philosophy of everyone for himself. Its the competition for resources that brings in the latest technology, innovations and overall better services. Anyone who believes that one would give up their own comfort for people who can't help themselves is delusional. Saying 'Bihar' ailments are due to lack of funds is idiotic because you wouldn't know how much is getting siphoned off behind the doors. I would suggest you to elect people who are inclined towards development and not some petty popular politics. As for the money, as and when development sets in, it would find its way to you.