Updated: 18-Jul-2019
This is the Indian Space Research Organization. they mainly build solid fuel rockets but also some with liquid fuels:
-The VSSC use solid fuel, S-7, S-9, S-125 and S-139 models with HTPB.
-The SLV-1 are very powerful and run on solid fuel with a thrust of 51,251 Kgf for 49 seconds. They are from the year 1997
-The SLV-2 is a solid rocket engine with a thrust of 27,227 Kgf.
-The SLV-3 runs on solid fuel with a thrust of 9,249 Kgf.
-The SLV-4 uses solid fuel as well and has a thrust of 2,736 Kgf.
The PSLV-1 was more powerful with a thrust of 495,590 Kgf for 97 seconds. It was used for PSLV and GSLV vehicles.
-The PSLV-3 rocket engine has a thrust of 33,519 Kgf for 75 seconds.
-The PSLV-4 delivered only 741 Kgf, but for 425 seconds.
-The liquid fuel engines would be, for example the LPSC like the L-40, the L-37.5, L-2 and PL-40. They use UDMH/N2O4.
-And there are those that used "cryo" fuel (cryogenic) like the C-12 engines, which used LH2 and LOX.
From Appendix 9: It's the India Space and Research Organization.
-They develop and build rocket engines:
-PSLV-1
-PSLV-3
-PSLV-4
-RH-125
-RH-125S
-RH-200
-RH-300
-RH-300-II
-RH-560
-RH-75
-SLV-1
-SLV-2
-SLV-3
-SLV-4
From Appendix 10: It is the Indian Space and Research Organization.
-In terms of engines, which is what interests us in this publication, first there are the Vikas engines.
"The Vikas are derived from the French Vikings"
“Vikas engine”
“Vikas 1”
“ISRO CE-7.5”
"The CE-7.5 on the LVM5-K shuttle"
"First ISRO liquid-fuel engine cluster design"
-Cluster of two Vikas engines in the first ISRO vehicle.
Engines of ISRO
Model: CE-20
Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:
Model: CE-60
Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:
Model: CE-7.5
Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:
Model: LVS
Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:
Model: Prithvi
Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:
Model: PSLV-1
Arquitecture: Rocket engine
Chambers:
Fuels:
Feed System:
Ignition:
Thrust: 495590 Kgf
Weight:
495,590 Kgf for 97 seconds
Model: PSLV-3
Arquitecture: Rocket engine
Chambers:
Fuels:
Feed System:
Ignition:
Thrust: 33519 Kgf
Weight:
33,519 Kgf for 75 seconds.
Model: PSLV-4
Arquitecture: Rocket engine
Chambers:
Fuels:
Feed System:
Ignition:
Thrust: 741
Weight:
741 Kgf during 425 seconds
Model: RH-125 VSSC
Arquitecture: Rocket engine
Chambers:
Fuels: HTPB
Feed System:
Ignition:
Thrust:
Weight:
Model: RH-125S VSSC
Arquitecture: Rocket engine
Chambers:
Fuels: HTPB
Feed System:
Ignition:
Thrust:
Weight:
Model: RH-200
Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:
Model: RH-300
Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:
Model: RH-300-II
Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:
Model: RH-560
Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:
Model: RH-75
Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:
Model: S-139 solid
Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:
Model: SCE-200 (RD-810)
Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:
Model: SLV-1
Arquitecture: Rocket engine
Chambers:
Fuels:
Feed System:
Ignition:
Thrust: 51251 Kgf
Weight:
51251 Kgf during 49 seconds
Model: SLV-2
Arquitecture: Rocket engine
Chambers:
Fuels:
Feed System:
Ignition:
Thrust: 27227 Kgf
Weight:
Model: SLV-3
Arquitecture: Rocket engine
Chambers:
Fuels:
Feed System:
Ignition:
Thrust: 9249 Kgf
Weight:
Model: SLV-4
Arquitecture: Rocket engine
Chambers:
Fuels:
Feed System:
Ignition:
Thrust: 2736 Kgf
Weight:
Model: Vikas X
Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:
Model: Vikas-2, -2B
Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:
Model: Vikas-4, -4B
Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight: