NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Controlling the dimensions and orientation of impinging propellant sheets in liquid rocket engine injectors.Working equations for dimensions and orientation of impinging propellant sheets in liquid rocket engine injectors
Document ID
19670033217
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Riebling, R. W.
Date Acquired
August 3, 2013
Publication Date
November 1, 1966
Publication Information
Publication: JOURNAL OF SPACECRAFT AND ROCKETS
Subject Category
Auxiliary Systems
Accession Number
67A11946
Distribution Limits
Public
Copyright
Other
Keywords
FUEL INJECTION
OXIDIZER
SPATIAL ORIENTATION
JET IMPINGEMENT
LIQUID PROPELLANT ROCKET ENGINE

Available Downloads

There are no available downloads for this record.

Related Records

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