TECHNOLOGY FEASIBILITY SPACECRAFT (TFS) TECHNOLOGY REPORT. VOLUME III. THERMAL ANALYSIS AND TEST.
Abstract
This report delineates the development and application of three analytical models simulating the thermal behavior of the TFS test vehicle in three modes; (1) cruise mode without radioisotope thermoelectric generator (RTG), (2) cruise mode with RTG, and (3) deorbit mode.
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 01, 1968
- Accession Number
- AD0670723
Entities
Organizations
- Martin Marietta