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regeneratively cooled combustion chamber

См. также в других словарях:

  • Regenerative cooling (rocket) — Regenerative cooling in rockets is where some or all of the propellant is passed through tubes, channels or otherwise in a jacket around the combustion chamber or nozzle to cool the engine because the fuel in particular and sometimes the oxidiser …   Wikipedia

  • Merlin (rocket engine) — Merlin 1C SpaceX Merlin 1A (shown) Country of origin United States Manufacturer SpaceX Liq …   Wikipedia

  • GIRD — Russian Group of Study of Reactive Motion (in Russian: Группа изучения реактивного движения (ГИРД), transliterated GIRD) was a Soviet research bureau founded in 1931 to study various aspects of rocketry, which was later incorporated into the… …   Wikipedia

  • Robert H. Goddard — Infobox Engineer image width = 150px caption =Robert Hutchings Goddard (1882 1945) name = Robert H. Goddard nationality = United States birth date = October 5, 1882 birth place = Worcester, Massachusetts death date = August 10, 1945 death place …   Wikipedia

  • RP-1 — (alternately, Rocket Propellant 1 or Refined Petroleum 1) is a highly refined form of kerosene outwardly similar to jet fuel, used as a rocket fuel. Although having a lower specific impulse than liquid hydrogen (LH2) and thus less thrust per unit …   Wikipedia

  • Bereznyak-Isayev BI-1 — infobox Aircraft name =Bereznyak Isayev 1 type =Fighter manufacturer =OKB 293 caption =The BI 1 designer =A.Y.Bereznyak and A.M.Isayev first flight =15 May 1942 retired =9 March 1945 primary user =Soviet Air Force number built =9Soviet research… …   Wikipedia

  • NK-33 — Role: 1st stage multi engine Propellants: RP 1/LOX Development year: 1970 s Overall dimensions Height 3.7 m (12 ft) Diameter …   Wikipedia

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