Voyager spacecraft phase B, task D. Volume 4 - Engineering tasks. Book 1 - Effect of capsule RTG'S on spacecraft Final report
Effect of radioisotope thermal generators in flight capsule on Voyager spacecraft configuration
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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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Voyager capsule engine system design considerations single versus multiple engine configuration
Single versus multiple engine configurations for Voyager capsule bus propulsion
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A large containment capsule for nuclear reactor irradiation of explosive materials
Large containment capsule for nuclear reactor irradiation of explosive materials
Avrami, L.↗
Soft lander, part 1 - Mars soft lander capsule study /entry from orbit/ - Summary
Selection of capsule for 1973 launching of Mars soft lander mission
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Soft lander, part 2 - Mars soft lander capsule study /entry from orbit/ - Introduction and parametric studies
Mission and systems parametric studies for Mars soft lander to define entry and landing capsule suitable for Mars probe in 1970 time period
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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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Wind-tunnel measurements of transition on the face of a blunt entry capsule at angle of attack.
Boundary layer transition point on forward portion of blunt Apollo type entry capsule model measured in high Reynolds number wind tunnel
Jones, R. A.↗
Thermal control of a Mars entry capsule.
Thermal control of Mars entry capsule with fiberglass honeycomb sandwich shell analyzed with and without aft thermal curtain, emphasizing cruise-flight phase
Stultz, J. W.↗
Development of a chemical heater for a Mars rough-landing capsule
Chemical reaction heater for Mars rough-landing capsule
Gram, M. B.↗
Evaluation of vacuum UV detector-spectroscopy systems for capsule reentry measurements
Vacuum ultraviolet detector-spectroscopy systems for capsule reentry measurements
Cann, M. W. P.↗
Titan/Mars Hard Lander. Volume 1 - 1400 Lb Capsule System Design Study
Mission definition and design study for 1400 lb hard lander Titan/Mars capsule system
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Titan/Mars hard lander. Volume 2 - Autonomous capsule system design study
Autonomous capsule system design study for Titan/ Mars hard lander
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Soft lander. Part 9 - Mars soft lander capsule study /entry from orbit/ analysis of inflatable landing systems
Analysis of inflatable landing systems - Mars soft lander capsule study
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Modification of government owned thermionic lead capsule TIE-I-3 Final report, 19 Jul. 1967 - 20 Sep. 1968
Government owned thermionic diode capsule design modification
Long, J. D.↗
Evaluation of configuration changes on optimum structural designs for a Mars entry capsule
Optimum structural design for Martian entry capsule configurations
Cohen, G. A.↗