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
The ignition transient in solid propellant rocket motors.Ignition pressure transient in solid rocket motors, examining chamber filling interval, flame propagation, heat transfer correlation, burning area, etc
Document ID
19670037784
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Most, W. J.
Parker, K. H.
Summerfield, M.
Date Acquired
August 3, 2013
Publication Date
August 1, 1966
Publication Information
Publication: ASTRONAUTICA ACTA
Subject Category
Propulsion Systems
Accession Number
67A16513
Distribution Limits
Public
Copyright
Other
Keywords
TRANSIENT PRESSURE
SOLID PROPELLANT ROCKET ENGINE
BURNING RATE
COMBUSTION TEMPERATURE
FLAME PROPAGATION
CONVECTIVE HEAT TRANSFER
CHAMBER PRESSURE

Available Downloads

There are no available downloads for this record.

Related Records

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