1 |
MIL-STD-1290A, "Light Fixed and Rotary-Wing Aircraft Crash Resistance," U.S. Department of Defense, Sept. 1988.
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2 |
Zimmermann, R.E., et al., "Aircraft Crash Survival Design Guide," USAAVSCOM TR 89-D-22 Volumes 1-5, Dec. 1989.
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3 |
Crocco, J., et al., "Full Spectrum Crashworthiness Criteria," Aircraft Survivability, Joint Aircraft Survivability(JAS) Program Office, pp 14-15, Spring 2009.
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4 |
Burrows, L.T., "Variable Design Criteria for Rotary Wing Aircraft Crash Resistance," Proceedings of the AHS 49th Annual Forum, May 1993.
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5 |
Carper, C.H. and Burrows, L.T., "Evolving Crashworthiness Design Criteria," Proceedings of the Energy Absorption of Aircraft Structures as an Aspect of Crashworthiness Conference, 1988.
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6 |
Burrows, L.T., "Proposed Revisions to MIL-STD-1290 Rotary Wing Aircraft Crash Resistance," Proceedings of the 18th European Rotorcraft Forum, Sept. 1992.
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7 |
Labun, L.C., "Rotorcraft Crash Mishap Analysis," U.S. Army RDECOM, Sept. 2009.
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8 |
Crocco, T., et al., "Full Spectrum Crashworthiness Criteria for Rotorcraft," U.S. Army RDECOM, Dec. 2011.
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9 |
Army Regulation 385-40, "Accident Reporting and Records," Department of Army, USA, April 1993.
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