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
Astro-1
LOx/LH2 propellant rocket stage. Engines 1 x M-1 plus 2 x J-2.

Status: Study. Thrust: 8,820.00 kN (1,982,810 lbf). Gross mass: 302,183 kg (666,199 lb). Unfuelled mass: 32,558 kg (71,778 lb). Specific impulse: 410 s. Specific impulse sea level: 345 s. Height: 29.00 m (95.00 ft). Span: 18.60 m (61.00 ft).



Country: USA. Engines: M-1. 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