| |
- Developmental
flights completed with successful third developmental launch in
March 1996.
- IRS-1D
launched by PSLV-C1 on September 29, 1997.
-
Now available for launching 1,000-1,200 kg class of remote sensing
satellites into polar sun-synchronous orbit.
-
IRS-P4 (OCEANSAT)
and two piggy back small satellites - Korean KITSAT and German TUBSAT launched by PSLV-C2 on May 26,1999.
-
Technology Experiment Satellite (TES) of ISRO, BIRD of Germany and PROBA of Belgium - into their intended orbits launched by PSLV-C3 on October 22, 2001.
-
The 1060 kg KALPANA-1 satellite - into a Geosynchronous Transfer Orbit (GTO) launched by PSLV-C4 on September 12, 2002.
- RESOURCESAT-1 (IRS-P6) satellite launched by PSLV-C5 on October 17, 2003.
- CARTOSAT-1 and HAMSAT satellites launched by PSLV-C6 on May 5, 2005.
Weight (t) : 294
Payload (kg) : 1000-1200
Height(m) : 44.43
Orbit : Polar orbit
| |
Stage-1 |
Stage-2 |
Stage-3 |
Stage-4 |
| Nomenclature |
Core
PSI + Strap-on PSOM 6Nos. |
PS2 |
PS3 |
PS4 |
| Propellant
|
Solid
HTPB Based |
Liquid
UDMH+ N2O4 |
Solid
HTPB Based |
Bi-Prop
MMH + N2O4 |
| Propellant
Mass (tonnes) |
138.0
+ 6X9.0 |
40.6 |
7.2
|
2.0 |
| Stage
Mass (tonnes) |
229
|
46
|
8.4
|
2.89 |
| Max
Thrust (kN) |
4628
+ 662 x 6 |
725
|
340
|
7.4
x 2 |
| Burn
time (sec) |
107.4
45 |
163
|
76
|
415 |
| Stage
Dia(m) |
2.8
1.0 |
2.8 |
2.0
|
1.3 |
| Stage
Length(m) |
20
10 |
12.5
|
3.6
|
2.1 |
| Control
|
SITVC
for Pitch & Yaw, Reaction control Thrusters for roll. SITVC
in 2 PSOMs for roll control augmentation |
Engine
Gimbal for Pitch & Yaw, Hot Gas Reaction Control Motor for
roll control |
Flex
Nozzle for Pitch & Yaw, PS4 RCS for roll control |
Engine
Gimbal for Pitch, Yaw and roll On -off RCS for coast phase
control |
|
