NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Pneumatic logic rocket engine sequence control.Fluidic breadboard version of rocket engine sequence control, describing pneumatic logic package and general limitations
Document ID
19670055252
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Milleman, S. E.
Date Acquired
August 3, 2013
Publication Date
July 1, 1967
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 67-518
Report Number: AIAA PAPER 67-518
Accession Number
67A33981
Funding Number(s)
CONTRACT_GRANT: NAS8-19
Distribution Limits
Public
Copyright
Other
Keywords
FLUIDICS
LOGIC CIRCUIT
CIRCUIT BOARD
PNEUMATIC CONTROL
ROCKET ENGINE CONTROL
SEQUENTIAL CONTROL

Available Downloads

There are no available downloads for this record.
No Preview Available