Paper
11 August 1998 Joint helmet-mounted cueing system (JHMCS) helmet qualification testing requirements
Garry W. Orf
Author Affiliations +
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.
© (1998) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Garry W. Orf "Joint helmet-mounted cueing system (JHMCS) helmet qualification testing requirements", Proc. SPIE 3362, Helmet- and Head-Mounted Displays III, (11 August 1998); https://doi.org/10.1117/12.317425
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Cited by 2 scholarly publications.
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KEYWORDS
Head

Signal attenuation

Safety

Resistance

Sensors

Calibration

Neck

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