HIGH-ALTITUDE REENTRY DRAG EFFECTS
Abstract
The effect of atmospheric drag on the trajectory of a reentry body is considered. The analysis is valid in the high altitude regime. Results are presented as the differential displacement and velocity from the vacuum trajectory for various values of ballistic coefficient.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1966
- Accession Number
- AD0634390
Entities
People
- S. Sharenson
Organizations
- MITRE Corporation