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An engine test stand is a facility used to develop, characterize and test engines. The facility, often offered as a product to automotive OEMs , allows engine operation in different operating regimes and offers measurement of several physical variables associated with the engine operation.
A rocket engine test facility is a location where rocket engines may be tested on the ground, under controlled conditions. A ground test program is generally required before the engine is certified for flight. Ground testing is very inexpensive in comparison to the cost of risking an entire mission or the lives of a flight crew.
Beal Aerospace was a launch vehicle development company founded in February 1997 by Andrew Beal, president of Beal Bank in Dallas, Texas. Headquartered in Frisco, Texas, [1] the goal of the company was to build and operate a privately developed heavy lift orbital launch vehicle. It ceased operations on October 23, 2000.
The P4-1 (a.k.a. LR64) engine was also manufactured for the AQM-37A target drone. [15] The engines and components were evaluated at an on-site test area located approximately one mile from the plant. Rocketdyne closed the plant in 1968. The plant has been used by several different companies for the refurbishment of jet aircraft engines.
On March 23, 1990, Allison's GMA 3007 was selected to power the Embraer EMB-145 regional jet. [2] In September 1990, it was selected for the Cessna Citation X. [1] The engine was first ground tested in mid-1991. [3] On August 21, 1992, the engine had its first test flight on a Cessna Citation VII testbed aircraft. [4]
Fairey Jet Gyrodyne – Jet-powered rotor technology demonstrator; Folland Fo.108 – Engine test bed; General Aircraft GAL.56 – Tailless swept wing glider; Gloster E.28/39 – Jet engine research; Gloster Meteor F8 "Prone Pilot" – Prone position flight control research; Gloster Trent Meteor – Turboprop propulsion
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The tests require engine manufacturers to carry out at least two tests of the engine, to make sure that the engine can survive a compressor or fan blade breaking off within the engine and a turbine blade breaking off within the engine, without fragments being thrown through the outside enclosure of the engine, creating a contained engine failure.
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