Spacecraft attitude control during thrusting maneuvers - Space vehicle design criteria /Guidance and control/
Systems design criteria for spacecraft attitude control during thrusting maneuvers
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Systems design criteria for spacecraft attitude control during thrusting maneuvers
Criteria and recommendations to ensure compatible interfaces between space vehicle structure and launch stand ground support equipment
Criteria and recommended practices for designing and testing flight separation mechanisms
Terrestrial environment /climatic/ criteria guidelines for use in NASA space vehicles and associated equipment development with major emphasis on Kennedy Space Center launch area
Description of design reference model for space shuttle propulsion system onboard checkout and monitoring equipment to establish design criteria - Vol. 2
Criteria and concepts for onboard checkout and monitoring system for space shuttle propulsion system - Vol. 3
Simulation studies for development of certification criteria applicable to SST takeoff and engine failure
Captive-fired testing of solid rocket motors for design criteria
Criteria and recommended practices for design, selection, analysis, and testing of deployable aerodynamic deceleration systems
Lubrication, friction, and wear processes analyzed for space vehicle design criteria
Design criteria for guidance and control spaceborne computer selection including physical and functional characteristics and reliability
Techniques for selecting performance criteria for voice, video, and digital data systems
Design criteria for passive gravity-gradient libration dampers
Accelerated life test models, criteria for model selection, and extrapolation in overstress models
Space communication system specification and performance criteria
Establishing solar cell array criteria for use as primary power source in lunar-based water electrolysis system
Design criteria for buckling prediction of elliptical and circular cylindrical shells under axial compression from asymmetric and axisymmetric shape imperfections distribution
Liquid fluorine feed system valves, seals and seats, discussing design criteria for flight weight components