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
Solid-propellant rockets.Burning rate, grain geometries and propulsion parameters derived for solid propellant rocket engines
Document ID
19650029851
Acquisition Source
Legacy CDMS
Document Type
Book Chapter
Authors
Lambert, C. H., Jr.
Date Acquired
August 2, 2013
Publication Date
January 1, 1964
Subject Category
Propulsion Systems
Accession Number
65A12555
Distribution Limits
Public
Copyright
Other
Keywords
PROPELLANT GRAIN
SPACECRAFT PROPULSION
SOLID PROPELLANT ROCKET ENGINE
BURNING RATE

Available Downloads

There are no available downloads for this record.

Related Records

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