Return launch and re-entry vehicles.
Manned lunar return launch and reentry vehicles, emphasizing spacecraft and system weight in relation to mission mode and propulsion
WEIGHT FACTOR↗
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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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Optimization of step rockets by the discrete maximum principle.
Optimum stage weight distribution in multistage rocket obtained by discrete maximum principle
MULTISTAGE ROCKET↗
Research and development of open-cycle fuel cells Fourth quarterly progress report, period ending Aug. 15, 1965
Digital computer program for minimizing weight of fuel cell power systems - prelaunch startup and instrumentation - mathematical model of static moisture removal process - fuel cell model
DIGITAL COMPUTER↗
Optimization of Saturn IB and V mounting and thermal conditioning panels Final report
Stress analysis for determining structural reliability of weight optimized mounting panel for Saturn launch vehicles
WEIGHT FACTOR↗
Catalogue of the meteorite collection
Catalog of meteorite collection listing locality, date, classification, number of specimens, and weight
METEORITE↗
Space vehicle water reclamation systems
Potential sources and methods description for space vehicle water recovery including mission weight penalties
WEIGHT FACTOR↗
Spacecraft capability for Apollo scientific experiments
Containers, storage compartments, and weight and volume distributions of scientific payloads aboard Apollo spacecraft for lunar exploration
APOLLO SPACECRAFT↗
Forecasts and appraisals for management evaluation, volume 2
Forecasting methodology for Apollo project - weight-performance data, mathematical models, probable error relationships, and manual to computational system
MATHEMATICAL MODEL↗
Application of low profile flange design for space vehicles
Low profile flange configuration with reduced size and weight for bolted separable connectors in space vehicles
WEIGHT FACTOR↗
Miniaturized tube fittings
Titantium alloy miniaturized flareless tube connectors with reduced weight and size for advanced space vehicles
WEIGHT FACTOR↗
Optimization of step rockets by the discrete maximum principle.
Optimum stage weight distribution in multistage rocket obtained by discrete maximum principle
WEIGHT FACTOR↗
Manned spacecraft design - The problems solved.
Problems of manned spacecraft design such as weight restriction, structural problems, heat protection, thermal control, vibration, etc
STRUCTURAL RELIABILITY↗
Strength of specimens containing parallel cylindrical holes.
Strength of ceramic specimens with parallel cylindrical holes, noting strength/weight characteristics during compression loading
CERAMIC BONDING↗
Minimum weight design aspects of stiffened cylinders under compression
Stiffener eccentricity and location influence on minimum weight design aspects of stiffened cylinders under compression
COMPRESSION LOADING↗
The requirements placed on electron tubes for space applications
Reliability, weight, and environment requirements of electron tubes for spacecraft application
COMPONENT RELIABILITY↗
Preliminary investigations to determine nuclear-electric spacecraft configurations for high-energy missions
Nuclear electric spacecraft configurations effects on mass of spacecraft radiation shield, heat rejection radiators, booster adapter, and aerodynamic shroud subsystems
WEIGHT FACTOR↗
Erectile antenna study Final report, 2 Mar. - 15 Sep. 1967
Optimum antenna weight distribution curves for six techniques to erect large aperture antennas
SPACE ERECTABLE STRUCTURE↗
Power system configuration study and reliability analysis. Spacecraft power system configuration reference manual
Preliminary power system configuration tradeoffs to select optimized systems with respect to reliability and weight - manual
MANUAL↗