VERTICAL RE-ENTRY OF VERY LIGHT-WEIGHT BODIES INTO THE EARTH'S ATMOSPHERE.
Abstract
The vertical re-entry of very light-weight bodies into the earth's atmosphere is studied. Rough approximations, an analytical method, and numerical integration are used to determine the velocity. It is found that below about 200,000 feet altitude the velocity is proportional to the sq. root of W/C(sub D)A when W/C(sub D)A is of the order of .10. The maximum deceleration increases linearly with increasing release altitude and it occurs at altitudes around 250,000 feet. Appreciable decelerations occur even for release altitudes of the order of 1,000,000 feet. It is found that the temperature of the thin external surfaces of light-weight bodies increases rapidly when the release altitude is increased. Extra material may be required locally in the detailed design, in order to reduce the surface temperature. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 01, 1967
- Accession Number
- AD0664027
Entities
People
- R. D. Linnell
Organizations
- General Dynamics