Analysis of Potential Plume Contamination Effects Resulting from Two 300-Lb. Bipropellant Engines Operating in a Satellite Environment.
Abstract
Two bipropellant rocket engines were analyzed for total plume contaminant production and a specific vehicular effect of the vehicle-deposited contaminant when operated with a prescribed satellite configuration and engine duty cycle. The two engines analyzed were the Rocketdyne RS-2101 and the Marquardt R 23-B. The vehicular effect analyzed was electrical power loss from degradation of the solar cell array.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1972
- Accession Number
- AD0746306
Entities
People
- J. R. Nunn
- R. J. Hoffman
- W. T. Webber