Encyclopedia Astronautica

Lox/Alcohol rocket stage. 35.00 kN (7,868 lbf) thrust. Mass 1,100 kg (2,425 lb).

No Engines: 4.

Status: Retired 1948.
Gross mass: 1,100 kg (2,400 lb).
Unfuelled mass: 500 kg (1,100 lb).
Height: 5.70 m (18.70 ft).
Diameter: 0.76 m (2.49 ft).
Thrust: 35.00 kN (7,868 lbf).
Burn time: 75 s.
Number: 3 .

More... - Chronology...

Associated Countries
Associated Engines
Associated Launch Vehicles
  • MX-774 American test vehicle. Project MX-774 inaugurated by AAF with Consolidated-Vultee to study rocket capabilities with an ICBM as a final objective. Limited funds permitted a few test launches. These rockets demonstrated technologies that woud later be applied to the Atlas. More...

Associated Manufacturers and Agencies
  • Convair American manufacturer of rockets, spacecraft, and rocket engines. Convair, USA. More...

Associated Propellants
  • Lox/Alcohol Liquid oxygen was the earliest, cheapest, safest, and eventually the preferred oxidiser for large space launchers. Its main drawback is that it is moderately cryogenic, and therefore not suitable for military uses where storage of the fuelled missile and quick launch are required. Alcohol (C2H5OH) was the fuel used for the German V-2 rocket, and the first derivative rocket engines in the United States, Soviet Union, and China used it as well. Better performance was achieved by increasing the alcohol concentration in the post-war engines. But after better-performance rocket-grade kerosene was developed by Rocketdyne in the REAP program of 1953, use of alcohol was abandoned. More...

Home - Browse - Contact
© / Conditions for Use