Voyager design studies. volume v- lander design, part i
Engineering and conceptual design of landing system for Voyager unmanned spacecraft
UNMANNED SPACECRAFT↗
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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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Surveyor lunar roving vehicle, phase I. Volume III - Preliminary design and system description. Book 2 - Validation of preliminary design Final report
Validation of preliminary design for Surveyor lunar roving vehicle - mobility, structure, deployment, folding and erection mechanism, and Apollo support scientific experiments
SURVEYOR PROJECT↗
Constricted high enthalpy arc heater design and performance data, including calculations for a 10 MW design First interim technical report
Performance prediction and design analysis of constricted coaxial-flow arc air heaters for materials testing and atmospheric entry simulation
ARC HEATING↗
Voyager spacecraft system. Preliminary design, volume A /book 2 of 4/ - Flight spacecraft preferred design - Telecommunications
Telecommunication system requirements and design for Voyager spacecraft 1971
VOYAGER PROJECT↗
Voyager spacecraft system. Preliminary design, volume A /book 4A of 4/ - Flight spacecraft preferred design - Implementation
Voyager project organization, management, scheduling and implementation of spacecraft design, and support scheduling
PROGRAM MANAGEMENT↗
Voyager spacecraft system. Preliminary design, volume B /book 2 of 3/ - Alternate designs considered - Telecommunications
Voyager spacecraft trade-off design parameters in telecommunication subsystems and between telecommunication system and other systems - data encoder and data storage systems
VOYAGER PROJECT↗
Voyager spacecraft system. Preliminary design, volume C - 1971 operational support equipment design
Operational support equipment design for Voyager spacecraft - system test and launch complex equipment
LAUNCH COMPLEX↗
Voyager spacecraft system - Preliminary design. 1969 test spacecraft design, volume D
Spacecraft functional description, mission objectives, design characteristics and system requirements of 1969 Voyager test flight
PROGRAM MANAGEMENT↗
Development of the Circuit Design from the Logic Design of a Random Walk Machine Final Report
Logic design of small, high speed, random walk machine for solving Laplace equation
LOGIC CIRCUIT↗
Preliminary design study of SLAMAST Scout- launched advanced materials and structures test-bed. Volume II - Design feasibility
Design feasibility of Scout launched recoverable lifting reentry vehicle test bed
REENTRY VEHICLE↗
Brayton-cycle radioisotope heat-source design study. Phase II /preliminary design/ report
Brayton cycle radioisotope heat source design
RADIOACTIVE ISOTOPE↗
Brayton-cycle radioisotope heat source design study. Phase I - /Conceptual design/ report
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↗
Voyager capsule, preliminary design, phase B. Volume III - Surface laboratory system. Section II - Preliminary design for OSE FINAL report
Operational support equipment and mission dependent equipment for preliminary design of surface laboratory portion of Voyager capsule bus system
PLANETARY SURFACE↗
Voyager capsule, preliminary design, phase B. Volume IV - Entry science package. Section II - Preliminary design for OSE FINAL report
Operational support equipment preliminary design for entry science package portion of Voyager flight capsule system
GROUND SUPPORT EQUIPMENT↗
Nondestructive testing for space applications - Feasibility and preliminary design study. Part 1 - Environmental testing, prototype hardware design, manufacture, and evaluation Final report
Feasibility of nondestructive testing in space environment - environmental testing, prototype hardware design, manufacture, and evaluation
Zoran, W. A.↗
Mercury/Gemini program design survey. NASA/ERC design criteria program stability, guidance and control
Mercury/Gemini stability, guidance, and control equipment design criteria
Source record↗
Zero Leakage Design for Ducts and Tube Connections for Deep Space Travel. Volume 4 - New Connector Designs and Testing Final Report, 5 Jul. 1963 - 30 Jun. 1967
Omega seal, diffusion bonded, pressure welded, and high temperature separable connector designs and environmental tests
Laniewski, J. P.↗
Isotope reentry vehicle design study - Conceptual design, phase 1A Topical report
Plutonium isotope reentry vehicle experimental design study
Source record↗