Apollo portable life-support system - development status.
Apollo space suit design including personal liquid cooling for conditioning and replenishing atmosphere inside space suit
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Apollo space suit design including personal liquid cooling for conditioning and replenishing atmosphere inside space suit
H-1, F-1, J-2 and RL-20 Apollo vehicle propulsion systems must have preflight design maturity due to man-rating requirement
Apollo capabilities extended for future biomedical, technological and operational experiments, trading space maneuvering capability for experiment load-carrying capacity
Guidance computer of Apollo guidance and navigation system discussing setup, keyboard console and memory design
Limited power and bandwidth transmission for portable camera of Apollo lunar television system
Schematic and flow diagrams showing uplink and downlink of Apollo spacecraft automatic checkout equipment
Vehicle assembly building, where propulsion and spacecraft stages are brought together, as key structure in Apollo-Saturn V prelaunch checkout operations
Theoretical and experimental data on Apollo command module /CM/ during water impact
Ground installations for development, qualification and checkout testing of Apollo space vehicle
Apollo entry radar acquisition of command module for tracking during ionization blackout
Omnidirectional radio antenna system design for Apollo command module
Space environment and meteoroid hazard to Apollo spacecraft - skin thickness estimate
Design analyses of physical and performance characteristics of unified Apollo S-band subsystems
Systems design analysis of unified S-band system for Apollo network - operations room equipment, performance evaluations, and equipment specifications
Impact acceleration and landing system characteristics of Apollo spacecraft command module configurations with deployed heat shield
Local buffeting response comparison between actual Apollo boiler plate service module and aeroelastic wind tunnel model - structural vibrations
Handling qualities for pilot control of Apollo lunar landing spacecraft
Computer derived orbital parameter variations for forty hour period after insertion into two reference Apollo lunar parking orbits