NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Data reduction and performance determinationDefinitions, algorithms, and procedures for the reduction of monopropellant thruster measurements to performance parameters are provided. A brief discussion of acquisition and recording systems is also included. Emphasis is placed upon monopropellant hydrazine engines, and some parameters relate specifically to the catalytic decomposition of hydrazine (e.g., percent ammonia dissociation). Performance of other types of monopropellant thrusters may, however, be determined by using procedures similar to those discussed. Two appendixes are included: (1) theoretical performance of monopropellant hydrazine; and (2) calculation of rotational performance.
Document ID
19790022118
Acquisition Source
Legacy CDMS
Document Type
Other
Date Acquired
August 9, 2013
Publication Date
June 1, 1979
Publication Information
Publication: Handbook of Recommended Practices for the Determination of Liquid Monopropellant Rocket Engine Performance
Subject Category
Spacecraft Propulsion And Power
Accession Number
79N30289
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Document Inquiry

Available Downloads

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