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Razor USA LLC, better known as Razor, is an American designer and manufacturer of manual and electric scooters, bicycles, and personal transporters. The company was founded in Cerritos, California in 2000 by Carlton Calvin and the JD Corporation. [1] Razor also owns the RipStik, Sole Skate, and Pocket Pros brands. [2]
National Launch System: NASA: 1991 1992 Black Horse: Mitchell Burnside Clapp 1993 1996 Kankoh-maru: Japanese Rocket Society K-1: Rocketplane Kistler: 1994 2007 Roton: Rotary Rocket: 1996 2001 Magnum: NASA: 2004
The SRMU is a three-segment solid rocket motor. Each segment has a casing wound from graphite fibre composite and an insulation system of EPDM rubber and kevlar. [1] The casing is filled with a fuel grain composed primarily of ammonium perchlorate and aluminium, joined by a HTPB binder. [2]
Engine Origin Designer Vehicle Status Use Propellant Power cycle Specific impulse (s) [a] Thrust (N) [a] Chamber pressure (bar) Mass (kg) Thrust: weight ratio [b] Oxidiser: fuel ratio
The AH-1G Cobra and the UH-1B "Huey" used a variety of launchers including the M158 seven-tube and M200 19-tube rocket launchers designed for the Mk 40 rocket motor; however, these models have been replaced by upgraded variants in the U.S. Marine Corps because they were not compatible with the Mk 66 rocket motor. The Hydra 70 rocket system is ...
The RS-68 (Rocket System-68) was a liquid-fuel rocket engine that used liquid hydrogen (LH 2) and liquid oxygen (LOX) as propellants in a gas-generator cycle. It was the largest hydrogen-fueled rocket engine ever flown. [3] Designed and manufactured in the United States by Rocketdyne (later Pratt & Whitney Rocketdyne and Aerojet Rocketdyne).
The ACES upper stage—fueled with liquid oxygen (LOX) and liquid hydrogen (LH 2) and powered by up to four rocket engines with the engine type yet to be selected—was a conceptual upgrade to Vulcan's upper stage at the time of the announcement in 2015. This stage could be upgraded to include Integrated Vehicle Fluids technology that would ...
It is the version for the Soyuz 2.1b and Soyuz 2.1v Block I stage. It is the first liquid rocket engine designed in Russia after the Soviet period. [3] [citation needed] RD-0124A It is the version that powers the Angara URM-2, both the 1.2 and the bigger 5 versions. It differs on the base model in having an extended burn time of 424 seconds and ...
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