Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
GSLV-3 stage
Part of N1 Block R
LOx/LH2 propellant rocket stage. The stage finally reached hardware status as a joint Russian-Indian development for India's GSLV booster.

AKA: Geostationary Satellite Launch Vehicle. Status: Active. Thrust: 75.05 kN (16,872 lbf). Gross mass: 14,600 kg (32,100 lb). Unfuelled mass: 2,200 kg (4,800 lb). Specific impulse: 460 s. Burn time: 675 s. Height: 8.72 m (28.60 ft). Diameter: 2.80 m (9.10 ft). Span: 2.80 m (9.10 ft).



Country: India. Engines: RD-56M. Launch Vehicles: GSLV. Propellants: Lox/LH2.

Back to top of page
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2019 Mark Wade - Contact
© / Conditions for Use