Monday, 6 January 2014

No Kudos to ISRO



courtsy-ISRO



Not much is being harped upon success of GSLV-D5 by ISRO and rightly so.It is a step forward 

after many steps back. It is not still commercially viable i.e. no agency or country will 

put it's money on it's satellite launch by GSLV.  Minimum of three more successful 

GSLV launches can only put ISRO as a front runner.


             A cryogenic rocket engine is an engine  that uses cryogenic fuel  , that is, its 

fuel or oxidizer (or both) are gases liquefied and stored at very low temperatures

to cool the propellants down to sub zero temperatures , converting them to liqiud 

form.
The cryogenic rocket engine provides more thrust than conventional liquid rocket  engines but the fuel and oxidizer needs to be super cooled in order to keep them in  a liquid state.
There is also a difference between the PSLV and GSLV in terms of the rocket itself. The PSLV has 4 stages that alternate between solid and liquid fuels while the GSLV has three stages with the only the first stage having solid fuel.


Geosynchronous Satellite Launch Vehicle (abbreviated as GSLV)

launch its satellites indigenously without dependence on foreign aid. GSLV has 

attempted eight launches to date, since its first launch in 2001 . Three launches have 

been successful, four have failed, and one was a partial failure, placing the satellite 

into an unplanned, but recoverable, orbit. The most recent flight, GSLV-D5 was 

launched successfully on 5 January 2014 during its second attempt.

Two launches in 2010 both failed; the first, in April, was the first flight of the GSLV 

Mk.II, with an Indian-developed third stage engine replacing the Russian engine used 

on earlier flights. The third stage failed to ignite. The next launch, in December, used 

the Russian engine, however the vehicle went out of control during first stage flight 

and was destroyed by range safety.

Problems with the connectors had occurred before – including one snapping in 

Russian built interstage adaptor  during the launch of INSAT-4CR which was 

responsible for the underperformance of that launch by  GSLV-F04. .

The  probable success rate of GSLV is put to be 0.29 (29%) by NASA.