(Translated by https://www.hiragana.jp/)
X-265

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
X-265
Hercules solid rocket engine. Sprint ABM first stage.

AKA: Sprint ABM-1;Sprint X265. Status: Retired 1992. Gross mass: 4,000 kg (8,800 lb). Burn time: 1.20 s. Height: 3.00 m (9.80 ft). Diameter: 1.37 m (4.49 ft).



Subtopics

Squirt-1 Solid propellant rocket stage.

HIBEX engine Boeing solid rocket engine. HIBEX first stage.

Upstage engine Boeing solid rocket engine. Upstage first stage.

Country: USA. Launch Vehicles: Sprint ABM, HEDI. Propellants: Solid. Stages: X-265. Agency: Hercules.

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