ENTRY OF SPACE VEHICLES INTO PLANETARY ATMOSPHERES. PART II. LIFTING ENTRY
Abstract
Closed-form expressions based on the approximations of P. Levine (Analysis of Re-entry Problems Associated with the Return of Manned Space vehicles to Earth, Avco RAD-TM-62-2, 15 February 1962 for the peak heat rate, loads, integrated heating, and corridor depth are presented; each expression is found to be a function of only two independent parameters. Comparison of the approximate calculations with numeric results are also presented. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- May 31, 1962
- Accession Number
- AD0276371
Entities
People
- Philip Levine