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Proceedings Paper

Joint helmet-mounted cueing system (JHMCS) helmet qualification testing requirements
Author(s): Garry W. Orf
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Paper Abstract

The Joint Helmet-Mounted Cueing System (JHMCS) program will provide capability to cue high off-boresight (HOBS) weapons to the operator's line of sight and to confirm weapon sensor LOS for the US Air Force and US Navy (USN) aircrew. This capability will ensure the USAF and USN pilots a first shot opportunity. The JHMCS incorporates an ejection-compatible helmet-mounted display system that will be installed on F- 15, F-16, F/A-18, and F-22 aircraft. The JHMCS includes a flight helmet with display optics, miniature cathode ray tube, magnetic receiver unit, miniature camera, automatic brightness control sensor, and microcontroller. The flight helmet for JHMCS is based on the new lightweight HGU-55A/P. This paper describes the requirements for the helmet qualification tests including: windblast, ejection tower, hanging harness, centrifuge, mass properties, energy attenuation and penetration resistance, noise attenuation, visor characteristics, compatibility demonstration, sled/in- flight ejection, water survival, standard conditions and environment. The test objective, success criteria, equipment configuration, and data collection requirements for each test is discussed.

Paper Details

Date Published: 11 August 1998
PDF: 6 pages
Proc. SPIE 3362, Helmet- and Head-Mounted Displays III, (11 August 1998); doi: 10.1117/12.317425
Show Author Affiliations
Garry W. Orf, The Boeing Co. (United States)


Published in SPIE Proceedings Vol. 3362:
Helmet- and Head-Mounted Displays III
Ronald J. Lewandowski; Loran A. Haworth; Henry J. Girolamo, Editor(s)

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