Parametric analysis and conceptual design of a radioisotope-thermionic space power generation system
Parametric analysis and conceptual design of radioactive isotope thermionic space power generation system
RADIOACTIVE ISOTOPE↗
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Conceptual design study of a liquid-core nuclear rocket technical report no. 665
Liquid cooled nuclear rocket conceptual design - nucleonics and systems analysis
Nelson, S. T.↗
Parametric analysis and conceptual design of a radioisotope-thermionic space power generation system.
Parametric analysis and conceptual design of radio isotope-thermionic space power generation system
RADIOACTIVE ISOTOPE↗
Conceptual design studies of an advanced Mariner spacecraft. Volume I - Summary
Parametric analysis and conceptual design study summary for advanced Mariner space probe - flyby bus and lander configuration for Mars investigation
LANDING SYSTEM↗
Conceptual design studies of an advanced Mariner spacecraft. Volume III - Lander design
Conceptual design study of advanced Mariner space probe - Mars lander configuration
SPACECRAFT DESIGN↗
Conceptual design studies of an advanced Mariner spacecraft. Volume IV - Flyby bus design
Conceptual design study of advanced Mariner space probe - flyby bus design for Mars mission
SURVEYOR PROJECT↗
Conceptual design studies of an advanced Mariner spacecraft. Volume V - Development plan and cost
Conceptual design study of advanced Mariner space probe - development plan and cost estimate for flyby bus/lander on Mars mission
SPACECRAFT DESIGN↗
Conceptual design for Mobile Geological Laboratory position and heading fix system
Conceptual design of position fixing system for Mobile Geological Laboratory in Lunar Mobile Laboratory simulation
GEOLOGY↗
Conceptual design studies of an advanced Mariner Mars flyby/lander system.
Conceptual design and parametric evaluation of advanced Mariner flyby bus/lander mission to Mars in 1969 and 1971 launch opportunities
PLANETARY LANDING↗
Conceptual mechanization studies for a horizon definition spacecraft structures and thermal subsystem
Conceptual mechanization for horizon definition spacecraft structures and thermal subsystem - spin-stabilized, hexagonal cylinder for launch of two-stage Improved Delta /DSV-3N/
SPACECRAFT CONFIGURATION↗
Conceptual mechanization studies for a horizon definition spacecraft communications and data handling subsystem
Conceptual mechanization for horizon definition spacecraft communications and data handling subsystem
SPACECRAFT COMMUNICATIONS SYSTEM↗
Conceptual design study report
Conceptual design of Northrop V/STOL jet operations research supersonic aircraft
Source record↗
Soft lander, part 4 - Mars soft lander capsule study /entry from orbit/ - Conceptual design 1
Conceptual design 1 for capsule for Mars soft lander for 1973 launching
Source record↗
Soft lander, part 5 - Mars soft lander capsule study /entry from orbit/ - Conceptual design 2
Conceptual design 2 for capsule for Mars soft lander for 1973 launching
Source record↗
Soft lander, part 6 - Mars soft lander capsule study /entry from orbit/ - Conceptual design 3 and 4
Conceptual design 3 for capsule for Mars soft lander for 1973 launching
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Soft lander, part 7 - Mars soft lander capsule study /entry from orbit/ - Conceptual design 5
Conceptual design 5 for capsule for Mars soft lander for 1973 launching
Source record↗
Conceptual techniques for reducing parasitic current gain of lateral pnp transistors
Two techniques have been conceptually proposed as possible means of reducing parasitic beta in lateral p-n-p transistors. One method uses a degenerate substrate and high concentration P /plus/ guard-ring diffusion, another places the base contact at the center of an annular ring structure.
Gallagher, R. C.↗
Conceptual design and analysis of shadow shield systems for thermal protection of cryogenic propellants Interim report
Conceptual design and analysis of shadow shield systems for thermal protection of cryogenic propellants
Gabron, F.↗