I MIL-STD-81OD Downloaded from https://www.everyspec.com 19 July 1983 115 EEEMMES a. Sevy, R.W. qtc~mputerprogram for Vibration Prediction of Fighter Aircraft Equipment”. AFFDL-TR-77-101. November 1977. b. Hall, P.S. ‘Vibration Test Level Criteria for Aircraft Equipment‘t. AFWAL-TR-80-3119. December 1980. c. Lloyd, A.J.P., Duleba, G .S., and Zeeben; J .P. “Environmental Control System (ECS) Tianeient Analysis”. AFFDL-TR-77-102. October 1977. d. Dieckmann, A.C., et al. ,,Development of Integrated Environmental Control Systems Design for Aircraft”. AFFDL-TR-72-9. May 1972. Quartz, 1., Samuels, A.H., and Curtis, A-J. Study Of the Cost Benef~ts of Mission Profile Testing”. AFWAL-TR-81-3028.
1981, Burkhard, A.H., et al. “CERT AFwAL~Tfi-82-3085. Evaluation Program Final Report”. ., s. nF-15 AFDT&E High-Temperature Evaluation!f. AFFTC-TR-75-19. October Desert Test and Climatic Laboratory 1975. DTIC number AD S011345L. 9 . . METHOD 520.0 19 July 1983 520.0-24