6.1 Referenced Documents
- a. A. Dantowitz, G. Hirshberger, and D. Pravidlo, "Analysis of Aeronautical Equipment Environmental Failures," Air Force Flight Dynamics Laboratory, TR-71-32, May 1971.
- b. NATO STANAG 4370, Allied Environmental Conditions and Test Publication (AECTP) 230, Climatic Conditions.
- c. MIL-HDBK-310, Global Climatic Data for Developing Military Products. 23 June 1997.
- d. D. B. Meeker and Allan G. Piersol, "Accelerated Reliability Testing Under Vibroacoustic Environments in Reliability Design for Vibroacoustic Environments," American Society of Mechanical Engineers AMD Vol-9, New York, NY, 1974.
- e. R.G. Lambert, "Accelerated Fatigue Test Rationale," General Electric Co., NY, March 1980
- f. David Alan Bies, "A Review of Flight and Wind Tunnel Measurements of Boundary Layer Pressure Fluctuations and Induced Structural Response," NASA CR-626, Bolt Beranek and Newman Inc., for NASA Langley Research Center, Oct 1966.
- g. Jack M. Graham, "Summary of Missile Vibration Levels During Straight and Level Flight on Various Aircraft," Pacific Missile Test Center, Point Mugu, CA, EM-1030-008, August 1984.
- h. Michael G. Hatcher and James R. Bautch, "PRAT Thermal and Vibration Profile Development," Sverdrup Technology Inc. for Aeronautical Systems Division, Eglin AFB, January 1992.
- i. Terry Elliott, "Design Parameters of Reverberant Acoustic Chambers for Testing Air-Carried Missiles," TM-81-15, Pacific Missile Test Center, Point Mugu, CA, March 1981.
- j. Handbook for Dynamic Data Acquisition and Analysis, IEST-RD-DTE012.2, Institute of Environmental Sciences and Technology, Arlington Place One, 2340 S. Arlington Heights Road, Suite 100, Arlington Heights, IL 60005-4516; Institute of Environmental Sciences and Technology Website.
- k. Terry Elliott, "Impact of Periodic Functional Testing on Sequential Test Plans," TP-82-25, Pacific Missile Test Center, Point Mugu, CA, May 1982.
- l. MIL-HDBK-781, Reliability Test Methods, Plans, and Environments for Engineering, Development, Qualification, and Production, Handbook for, 1 April 1996.
- m. Michael T. Bunij, "SIDEWINDER Manufacturer Dependent Vibration Response Investigation," Pacific Missile Test Center, Point Mugu, CA, June 1989.
- n. U.S. Standard Atmosphere, 1976; DTIC No. ADA035728.
- o. D. F. Rex ed. "World Survey of Climatology," Elsevier, NY, 1969.
- p. Sharon A. Ogden, "A Mathematical Method for Determining Laboratory Simulation of the Captive Flight Vibration Environment," Proceedings of the 48th Shock and Vibration Symposium, Huntsville, AL, 1977.
6.2 Related Documents
- a. Egbert, Herbert W. “The History and Rationale of MIL-STD-810 (Edition 2),” January 2010; Institute of Environmental Sciences and Technology, Arlington Place One, 2340 S. Arlington Heights Road, Suite 100, Arlington Heights, IL 60005-4516
(Copies of Department of Defense Specifications, Standards, and Handbooks, and International Standardization Agreements are available online at https://assist.dla mil.
Requests for other defense-related technical publications may be directed to the Defense Technical Information Center (DTIC), ATTN: DTIC-BR, Suite 0944, 8725 John J. Kingman Road, Fort Belvoir VA 22060-6218, 1-800-225-3842 (Assistance--selection 3, option 2), http://www.dtic mil/dtic/; and the National Technical Information Service (NTIS), Springfield VA 22161, 1-800-553-NTIS (6847), http://www.ntis.gov/.
MIL-STD-810H METHOD 523.4, ANNEX A
METHOD 523.4, ANNEX A PHILOSOPHY OF TESTING, VIBRO-ACOUSTIC/TEMPERATURE TEST PROFILE DEVELOPMENT
- SCOPE.
1.1 Purpose.
This annex provides an example of the development of a Vibro-Acoustic/Temperature test profile.