The Wayback Machine - https://web.archive.org/web/20161228025343/http://astronautix.com/a/astrolaunchvehicle.html
Astro launch vehicle

Encyclopedia Astronautica
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 launch vehicle
Part of RTTOCV Family
ROOST and Astro

ROOST and Astro
Credit: NASA
American winged orbital launch vehicle. Douglas design of the early 1960's for a two-stage-to-orbit, winged, recoverable vehicle. Two versions were envisioned - a preliminary one the size of a DC-8 and a monster vehicle capable of delivering one million pounds payload to orbit. It was assumed at this scale that LOx/LH2 vehicles could achieve stage propellant mass fractions of 88% to 86%.
See More

AKA: Astro. Status: Study 1963. Payload: 454,500 kg (1,002,000 lb). Height: 270.00 m (880.00 ft). Span: 125.00 m (410.00 ft). Apogee: 325 km (201 mi).

LEO Payload: 454,500 kg (1,002,000 lb) to a 325 km orbit at 28.00 degrees.

Family: orbital launch vehicle, Winged. Country: USA. Agency: Douglas. Bibliography: 214.

Photo Gallery
AstroAstro
Credit: NASA
AstroAstro
Credit: NASA
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
� 1997-2016 Mark Wade - Contact
� / Conditions for Use