TRANSACTIONS OF THE SYMPOSIUM ON BALLISTIC MISSILE AND SPACE TECHNOLOGY (7TH) HELD AT THE UNITED STATES AIR FORCE ACADEMY, COLORADO, ON 13-16 AUGUST 1962. VOLUME I. SPACE VEHICLES AND SYSTEM DESIGN HYPERSONICS AND RE-ENTRY TECHNIQUES PROPULSION STRUCTURES AND MATERIALS MATHEMATICAL RELIABILITY TECHNIQUES
Abstract
Identifiers: Abort, Lunar surface vehicles, Attitude control systems, Flat plate models. Contents: Locomotion analysis of lunar surface vehicles; Penetration studies of simulated lunar dust; Sterilization of electronic components of spacecrafts; Injection conditions for earth-moon trajectories; Reuseability and disposal of nuclear systems in space; Self- luminous hypersonic wake radiation measurement and flow visualization; Ballistic missile decoy optimization - programming; Flat plate surface hypersonic heat transfer; Dielectrophoretic propellant orientation in zero gravity; Heat transfer and ablation in aftclosures of solid motors; Nuclear propulsion for orbit-based spacecraft; Oxidation protection of refractory metals in aerospace; A non-parametric technique for reliability comparisons; Failure prediction for nonmaintainable electronic components; and Reliability as a thermostructural design criterion.
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 01, 1962
- Accession Number
- AD0287836
Entities
Organizations
- The Aerospace Corporation