NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Integration of pyrotechnics into aerospace systemsThe application of pyrotechnics to aerospace systems has been resisted because normal engineering methods cannot be used in design and evaluation. Commonly used approaches for energy sources, such as electrical, hydraulic and pneumatic, do not apply to explosive and pyrotechnic devices. This paper introduces the unique characteristics of pyrotechnic devices, describes how functional evaluations can be conducted, and demonstrates an engineering approach for pyrotechnic integration. Logic is presented that allows evaluation of two basic types of pyrotechnic systems to demonstrate functional margin.
Document ID
19940025131
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bement, Laurence J.
(NASA Langley Research Center Hampton, VA, United States)
Schimmel, Morry L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1993
Publication Information
Publication: NASA. Ames Research Center, The 27th Aerospace Mechanisms Symposium
Subject Category
Propellants And Fuels
Accession Number
94N29634
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available