Thermal control for the Apollo lunar surface experiments package /ALSEP/.
Thermal control subsystem for Apollo lunar surface experiments package, noting construction and operation principles
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Thermal control subsystem for Apollo lunar surface experiments package, noting construction and operation principles
Apollo thermal control systems and concepts, discussing self-shadowing
Apollo lunar surface experiments package /ALSEP/ OF scientific instruments and supporting subsystems
Metrology requirements for Apollo project, noting control and measuring equipment and calibration procedures
Apollo lunar module /LM/ rendezvous radar system and tracking device
Model tests for determination of structural response of Apollo Command Module to water impact
Apollo manned lunar landings, system hardware, operational problems and development of lunar surface experiments package /ALSEP/
Manual thrust vector control development for Apollo Command and Service Module Stabilization and Control System
Apollo engineering simulation activity, particularly analog-digital real time hybrid simulation for guidance and control
Apollo Extension System for lunar surface missions, discussing extension of mission time by unmanned LEM laboratory
Base-mounted landing rocket system for Apollo type vehicle evaluated for heat-shield water pressure, ground effect, vehicle dynamics, etc
Design, tests, operation and limitations of Apollo man-rated environmental control system simulation chamber
Scan converter for Apollo TV performing time base conversion with destructive readout storage element and flicker correction with magnetic disk
Vibration response of Apollo shell structures to acoustic and aerodynamic noise
NASA STADAN and Apollo network antenna systems, analyzing tracking antenna systems, command systems and operational problems
Mechanical impact attenuation system for Apollo spacecraft provides stable land landing platform, noting deployed heat shields, extended legs, pneumatic bags, etc
Apollo manned space flight program including mission profile, spacecraft and constituent systems
Ground installations for development, qualification and checkout testing of Apollo space vehicle