Encyclopedia Astronautica
Sanger-Bredt


Lox/Kerosene propellant rocket stage. Loaded/empty mass 99,773/19,955 kg. Thrust 1,428.80 kN. Vacuum specific impulse 306 seconds.

Cost $ : 13.000 million.

Status: Study 1943.
Gross mass: 99,773 kg (219,961 lb).
Unfuelled mass: 19,955 kg (43,993 lb).
Height: 28.00 m (91.00 ft).
Diameter: 2.32 m (7.61 ft).
Span: 15.00 m (49.00 ft).
Thrust: 1,428.80 kN (321,207 lbf).
Specific impulse: 306 s.
Specific impulse sea level: 210 s.
Burn time: 168 s.

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Associated Countries
Associated Engines
  • Sanger-Bredt Notional Lox/Kerosene rocket engine. 1428.8 kN. Study 1943. Used in Sanger-Bredt. Isp=306s. More...

Associated Launch Vehicles
  • Saenger German sled-launched intercontinental boost-glide missile. Saenger-Bredt antipodal bomber - sled launched, boosted to suborbital velocity, 'skips' off upper atmosphere to deliver bombload on target, recovery back at launch site. Fascinated Stalin, led to US Dynasoar project. More...

Associated Propellants
  • Lox/Kerosene 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. In January 1953 Rocketdyne commenced the REAP program to develop a number of improvements to the engines being developed for the Navaho and Atlas missiles. Among these was development of a special grade of kerosene suitable for rocket engines. Prior to that any number of rocket propellants derived from petroleum had been used. Goddard had begun with gasoline, and there were experimental engines powered by kerosene, diesel oil, paint thinner, or jet fuel kerosene JP-4 or JP-5. The wide variance in physical properties among fuels of the same class led to the identification of narrow-range petroleum fractions, embodied in 1954 in the standard US kerosene rocket fuel RP-1, covered by Military Specification MIL-R-25576. In Russia, similar specifications were developed for kerosene under the specifications T-1 and RG-1. The Russians also developed a compound of unknown formulation in the 1980's known as 'Sintin', or synthetic kerosene. More...

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