COMPOUND A/HYDRAZINE ENGINE DESIGN STUDY. PART II. APPENDIXES.
Abstract
The results of the Compound A/Hydrazine Engine Design Study, including the parametric engine information needed to perform mission analyses for evaluation of advanced engine design concepts, are reported in two parts. Part 1 includes parametric engine performance, weight, envelope, and capability for numerous engine concepts utilizing various fuels and different technologies for the feed system, propellant injection, and chamber cooling systems. Part 2 is made up of six appendixes, which encompass a discussion of specific propellant characteristics, along with methods used in accomplishing performance, weight, and heat transfer calculations. In addition, those design methods for turbopumps and gas generators which are common to all engine concepts are discussed.
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 30, 1968
- Accession Number
- AD0390231
Entities
People
- C. Scott Henry
- Clayton W. Williams
- Clifford Paavola
- R. Verne Coats
- Werner P. Luscher
Organizations
- Aerojet Rocketdyne Holdings