GSLV Mk.I and Mk.II

GSLV
by WDGraham from Wikipedia

Country of Origin: India
Manufacturer: ISRO

Height: 49.13 m
Diameter: 2.8 m
Payload to LEO: 5 tons (GSLV Mk. II)
Total Mass: 414.75 tons

Launch Sites: Satish Dhawan
First Flight: April 18, 2001
Last Flight: Active
Total Launches: 9
Successful Launches: 4

 

 

GSLV Mk.Ia

Stage Diameter Fuel Engine Time Thrust (Vac.) ISP (SL / Vac.) Mass / Empty Mass
Boosters (L40) 2.1 m UDMH / N2O4 4 x Vikas 2149 s 4 x 760 kN 262 s / ?
1 (S-125) 2.8 m Solid S-125 100 s 4700 kN 237 s / ?
2 (L-37.5) 2.8 m UDMH / N2O4 Vikas 4150 s 800 kN ? / 295 s
3 (C-12) 2.8 m LH2 / LOX KVD-1M754 s 73.6 kN ? / 454 s
WordPress Table

 

 

GSLV Mk.II

Stage Diameter Fuel Engine Time Thrust (Vac.) ISP (SL / Vac.) Mass / Empty Mass
Boosters (L40H) 2.1 m UDMH / N2O4 4 x Vikas 2161 s 4 x 760 kN 262 s / ?
1 (S-139) 2.8 m Solid S-139 110 s 4700 kN 237 s / ?
2 (GS2) 2.8 m UDMH / N2O4 Vikas 4150 s 800 kN ? / 295 s
3 (CUS12) 2.8 m LH2 / LOX CE-7.5720 s 75 kN ? / 454 s
WordPress Table

 

 

Links:

b14643.de

Wikipedia

Destination Orbite

Space Launch Report

Encyclopedia Astronautica

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