DocumentCode :
1701563
Title :
Design of the GE aircraft engine compact range facility
Author :
Silz, R.
Author_Institution :
GE Aircraft Engines, Cincinnati, OH, USA
Volume :
4
fYear :
2001
Firstpage :
432
Abstract :
GE Aircraft Engines (GEAE) in Cincinnati, Ohio recently built a compact range facility to operate from 800 MHz to 18 GHz. The design process included visits to other recently completed facilities so that industry best practices could be incorporated into the design of the state-of-the-art facility. The facility includes a 30x30x65 ft. chamber, corner fed blended rolled edge reflector, Chebyshev multilevel absorbers, a 12 ft. diameter turntable and a rail mounted gantry crane for target mounting. Facility design, chamber, reflector, absorber, target handling and fire protection systems are discussed. The performance of the facility is discussed elsewhere (see Gupta, I.J. et al., AMTA 22nd Meeting and Symposium Proceedings, 2000). The facility was built to meet two primary objectives: (1) perform production acceptance testing of GEAE engine components; (2) to support advanced technology research and development programs.
Keywords :
aerospace engines; aerospace test facilities; conformance testing; design engineering; radar cross-sections; 12 ft; 30 ft; 65 ft; 800 MHz to 18 GHz; Chebyshev multilevel absorbers; GE aircraft engine; RCS test; compact range facility; corner fed blended rolled edge reflector; design process; facility design; fire protection systems; production acceptance testing; rail mounted gantry crane; target mounting; turntable; Aircraft propulsion; Best practices; Chebyshev approximation; Cranes; Fires; Performance evaluation; Process design; Production; Protection; Rails;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Antennas and Propagation Society International Symposium, 2001. IEEE
Conference_Location :
Boston, MA, USA
Print_ISBN :
0-7803-7070-8
Type :
conf
DOI :
10.1109/APS.2001.959491
Filename :
959491
Link To Document :
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