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Results for “DESIGN” Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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At least 775 records · Page 43NASA NTRS 1963
Off-design aerodynamic characteristics of swept arrow wings with twist and camber at supersonic velocities
NASA NTRS 1963
Design criteria for zero-leakage connectors for launch vehicles - plastic flow & flange rolling
NASA NTRS 1964
Role of spatial imagination in designing and in teaching of drawing in technical schools
NASA NTRS 1962
Contactor characteristics and power relay design for application in Saturn launch vehicle systems
NASA NTRS 1963
Engineering and design data for Voyager Mars and Venus lander systems
NASA NTRS 1963
Engineering and conceptual design of landing system for Voyager unmanned spacecraft
NASA NTRS 1964
Validation of preliminary design for Surveyor lunar roving vehicle - mobility, structure, deployment, folding and erection mechanism, and Apollo support scientific experiments
NASA NTRS 1965
Performance prediction and design analysis of constricted coaxial-flow arc air heaters for materials testing and atmospheric entry simulation
NASA NTRS 1965
Telecommunication system requirements and design for Voyager spacecraft 1971
NASA NTRS 1965
Voyager project organization, management, scheduling and implementation of spacecraft design, and support scheduling
NASA NTRS 1965
Voyager spacecraft trade-off design parameters in telecommunication subsystems and between telecommunication system and other systems - data encoder and data storage systems
NASA NTRS 1965
Operational support equipment design for Voyager spacecraft - system test and launch complex equipment
NASA NTRS 1965
Spacecraft functional description, mission objectives, design characteristics and system requirements of 1969 Voyager test flight
NASA NTRS 1966
Logic design of small, high speed, random walk machine for solving Laplace equation
NASA NTRS 1967
Design feasibility of Scout launched recoverable lifting reentry vehicle test bed
NASA NTRS 1967
Brayton cycle radioisotope heat source design
NASA NTRS 1967
Conceptual designs for radioisotope heat source systems to provide 25 kW thermal power to Brayton cycle power conversion system for space applications
ELECTRIC POWER CONVERSION ↗ NASA NTRS 1967
Operational support equipment and mission dependent equipment for preliminary design of surface laboratory portion of Voyager capsule bus system