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↗
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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
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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
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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
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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.↗
The conceptual design of a small solar probe /Sunblazer/
Conceptual design of Sunblazer space probe for determining electron density of solar corona
Baker, R. H.↗
Cost studies of Multipurpose Large Launch Vehicles. Volume 2 - Half size vehicle /MLLV/ conceptual design Final report
Conceptual design of half-size multipurpose large launch vehicle with liquid propellant main and injection stages and solid propellant strap-on stage
Corso, C. J.↗
A conceptual design of the space shuttle integrated avionics system
Conceptual design development of space shuttle integrated avionics system emphasizing necessary electronics systems
Digesu, F. E.↗
A fundamental approach to aircraft manufacturing cost estimating in the conceptual design phase
Aircraft manufacturing cost estimation in conceptual design phase, using structural synthesis program for cost buildup simulation
Gregory, T. J.↗
Malfunction Analysis of a Conceptual Space Power Fast-Spectrum Reactor
Potential malfunction analysis for conceptual lithium-cooled space power fast spectrum reactor
Peoples, J. A.↗