NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Ignition and ignition propagation in solid propellant motors.Solid propellant ignition and ignition propagation for rocket exhaust and hypergolic-type igniters
Document ID
19660054935
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anderson, R.
Brown, R. S.
Cose, D. A.
Jensen, G. E.
Date Acquired
August 3, 2013
Publication Date
June 1, 1966
Subject Category
Propellants
Accession Number
66A34225
Distribution Limits
Public
Copyright
Other
Keywords
CHAMBER PRESSURE
PROPELLANT COMBUSTION
SOLID PROPELLANT IGNITION

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available