This content is not included in your SAE MOBILUS subscription, or you are not logged in.
Requirements for Space Propulsion Systems
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1968 by SAE International in United States
Annotation ability available
Event: Space Technology Conference
This paper explores some of the many considerations which enter into the choice of a specific spacecraft propulsion system for a particular application. The environment and its influence on propulsion requirements are discussed in general terms, characteristics of several propellant combinations are presented and an example of a typical ambitious mission is used.
A general conclusion is that the state of the art of spacecraft propulsion technology must advance on a broad front in the time period prior to project definition in order to provide the technological options which allow significant optimization of the complete project propulsion system.
CitationWilcox, W. and Rollins, R., "Requirements for Space Propulsion Systems," SAE Technical Paper 680360, 1968, https://doi.org/10.4271/680360.
- Cumming J. M. “Rocket Space Propulsion in the 1970's.” SAE Transactions 77 1968 paper 680361
- Mathson J. C. “Flox/Light-Hydrocarbon Propellant Propulsion Research.” SAE Transactions 77 1968 paper 680362
- Gardner William N. Hook W. Ray “Earth Orbital Program Strategy.” SAE Transactions 77 1968 paper 680363
- “Manned Planetary Flyby Missions Based on Saturn/Apollo Systems.” Contract NAS8-18025 North American Aviation, Inc. 1 February 1967