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
Falcon 9-1
LOx/Kerosene propellant rocket stage. .

Status: Retired. Thrust: 4,433.00 kN (996,578 lbf). Gross mass: 264,000 kg (582,000 lb). Unfuelled mass: 13,000 kg (28,000 lb). Specific impulse: 304 s. Specific impulse sea level: 266 s. Burn time: 180 s. Height: 29.00 m (95.00 ft). Diameter: 3.66 m (12.00 ft). Span: 4.20 m (13.70 ft).



Subtopics

Falcon 9.1-1 LOx/Kerosene propellant rocket stage. .



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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use