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
XM-45
Rocket solid engine. Trailblazer 2 M second stage.

AKA: Trailblazer 2 M-2. Status: Retired 1966. Thrust: 200.00 kN (44,960 lbf). Gross mass: 900 kg (1,980 lb). Unfuelled mass: 377 kg (831 lb). Burn time: 6.00 s. Height: 4.50 m (14.70 ft). Diameter: 0.38 m (1.24 ft).

Country: USA. Launch Vehicles: RAM A, HJ PRV. Propellants: Solid. Stages: XM-45.
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