skip to main content
OSTI.GOV title logo U.S. Department of Energy
Office of Scientific and Technical Information

Title: Pyroshock: Bibliography

Conference ·
OSTI ID:6721627

This paper represents a review copy for text that is to be included in the Shock and Vibration Recommended Practice Document. This section on pyroshock is written an a general introduction to and description of the topic loading to presentation of an extensive bibliography on the subject. Pyroshock is an evolving science that needs continued focus on both achieving improvements in testing and measurement techniques and advancing instrumentation capabilities. When desired in the near future, recommended practices can be presented. Pyroshock phenomena are associated with separation systems of missiles. spacecraft, and in some cases airplanes. During launch, a rocket driven vehicle may be exposed to 19 to 30 g's of acceleration with predominant frequencies less than 200 Hz. After launch or takeoffs sections or parts of vehicles may be separated rapidly using explosive driven release mechanisms. Separations can involve stage disconnections for spacecraft sections or payload ejections from missiles and airplanes. At separation, localized pyrotechnic induced accelerations may range from 1000 to over 100,000 g's at frequencies much higher than 1000 Hz. These pyroshocks are characterized by high intensity, high frequency transients that decay rapidly. Pyroshock impulses have insignificant velocity changes.

Research Organization:
Sandia National Labs., Albuquerque, NM (United States)
Sponsoring Organization:
USDOE; USDOE, Washington, DC (United States)
DOE Contract Number:
AC04-76DP00789
OSTI ID:
6721627
Report Number(s):
SAND-93-0331C; CONF-930529-1; ON: DE93007605
Resource Relation:
Conference: 39. annual technical meeting of the Institute of Environmental Sciences, Las Vegas, NV (United States), 2-7 May 1993
Country of Publication:
United States
Language:
English