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
Nova GD-J-2
Part of Nova 2 stage series
LOx/LH2 propellant rocket stage. Massed estimated based on tank volumes, total thrust, and first stage burnout conditions.
Status: Study 1963. Thrust: 13,346.00 kN (3,000,300 lbf). Gross mass: 1,270,000 kg (2,790,000 lb). Unfuelled mass: 91,000 kg (200,000 lb). Specific impulse: 428 s. Burn time: 365 s. Height: 38.00 m (124.00 ft). Diameter: 19.50 m (63.90 ft). Span: 19.50 m (63.90 ft).
No Engines: 2.
Country:
USA.
Engines:
M-1.
Launch Vehicles:
Nova GD-J.
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