Dodge Satellite Performance 1 July 1967 - 1 October 1968. Volume A
Staging Loads - Space Vehicle Design Criteria
Spacecraft Sterilization Training Manual
Study of Structural-Thermal Insulation- Meteoroid Protection Integration
Integral Launch and Reentry Vehicle. Volume 2 - Technology Identification Final Report
Thermal Model of a 75 Watt/E/ Space Power Planar Rtg System
Spacecraft Charge Build-Up Analysis
Calculation of the Penetration Flux for a Multiwall Structure on the Lunar Orbiter Spacecraft
Calibration of Pegasus and Explorer 23 Detector Panels
ATM Star Tracker Vehicle Structure Occultation Study
Effects of Bottom-Structure Flexibility on Water Landing Loads of APOLLO Spacecraft Models
Heat Transfer Characteristics of a Spacecraft Propane Boiler System
Heatpipes and Vapor Chambers for Satellite Thermal Balance