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The Solid Rocket Motor Upgrade (SRMU) was a solid rocket motor that was used as a booster on the Titan IVB launch vehicle. Developed by Hercules (later ATK ), it was intended to be a high-performance, low-cost upgrade to the UA1207 boosters previously used on Titan IV.
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
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]
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 "Fénix" is a M4E1 tower, recovered from a car M42 Duster and 2 M50 machine guns .30 caliber for Protective Part (a cylindrical tower made of welded armor plate with open top with twin mounting Bofors 40 mm gun), mounted on a tactical platform Truck 6x6 2 + 1 ⁄ 2-ton Reo M-35.
The Hydra 70 is derived from the 2.75-inch (70 mm) diameter Mk 4/Mk 40 Folding-Fin Aerial Rocket developed by the United States Navy for use as a free-flight aerial rocket in the late 1940s. The Mk 40 was used during the Korean and Vietnam wars to provide close air support to ground forces from about 20 different firing platforms, both fixed ...
The FMTV's origins trace back to a U.S. Army Training and Doctrine Command requirements document issued in 1983 for a Medium Tactical Truck (MTT), the intended replacement for the in-service 2.5-ton truck. In July 1984, a program to look at a future 5-ton truck procurement to replace in-service 2.5- and 5-ton trucks began. Cost analysis ...
The Solid Fuel Ducted Ramjet is a missile propulsion system that includes a thrust modulated ducted rocket with a reduced smoke nozzle-less missile booster. [2] The thrust modulation in the system is achieved using a hot gas flow controller. [2] The system utilises a solid fuelled air-breathing ramjet engine.