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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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Elimination of permeation and bubble formation in Apollo RCS positive expulsion tankage
Environmental tests of design modifications for Apollo RCS positive expulsion tankage
Design of thermal control system for cryogenic fluid storage tanks
Analyzing thermal control system for B2H6/OF2 propulsion module
One way velocity increments obtainable from one and two stage propulsive configurations for expended and reusable modes - tables
Outbound and inbound stage weight requirements for planetary sample return mission payload and energy requirements - graphs
Surface evaluation of stainless steel gyro bearings manufactured by various hardening techniques
Test description and results for high Mach number transonic fan stages to determine range and distortion tolerance for various rotor tip casing treatment configurations
Tabulations of blade element and circumferential distortion flow data in tests of high Mach number transonic fan stages with various rotor tip casing treatment configurations
Handling of waste products on spacecraft to include identification, potential for on-board utilization, pretreatment requirements for storage, and disposal concepts - Vol.1
Thermochemical and thermophysical properties and ablation test data for three charring ablators
Effects of warp tension on stowed blanket dynamics and in-plane structural characteristics of rollup solar arrays
Concepts and requirements analysis for automated onboard checkout of manned space station
Language and executive software requirements for automated onboard checkout of manned space station
Technology for implementation of onboard electronics maintenance facility for manned space station
Failure effects analysis of guidance, navigation, and control, data management, and communications subsystems
Thermal, chemical, and wear properties of carbon-graphite seal ring materials at air temperature to 1300 F
Architectural design of spaceborne computer system operating in multi-element configuration