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
FastTrack
Notional LOx/Kerosene rocket engine. Design concept. NASA Marshall Space Flight Center prototype experimental engine that led to Fastrac low-cost engine for X-34.

Status: Design concept. Thrust: 44.10 kN (9,914 lbf). Specific impulse: 348 s. Burn time: 325 s. Diameter: 2.00 m (6.50 ft).

Country: USA. Propellants: Lox/Kerosene. Stages: X-34A-2.
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