Integral Launch and Reentry Vehicle System. Volume 3 - Program Plans and Costs
Program plans for design, manufacturing, development test, launch operations, and vehicle recovery
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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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The Applications Technology Satellite apogee rocket motor - A summary report
Design, testing, and development of solid propellant rocket engine for orbital transfer of Applications Technology Satellite
Anderson, R. G.↗
Apollo guidance, navigation and control - Design survey of the Apollo inertial subsystem
Design, development, and testing of inertial guidance and navigation systems for Apollo project
Jopling, P. F.↗
Development of a 60 kW alternator for SNAP-8
Design and development testing of 60 kW alternator for SNAP 8
Cherry, M. G.↗
A semi-active gravity gradient stabilization system
Semiactive gravity gradient attitude stabilization system /SAGS/ providing active pitch control and semipassive roll/yaw control, discussing design, development and testing
Redisch, W. N.↗
Alpha and X-ray spectrometers: Apollo lunar orbital science program
Design, development, fabrication, test, checkout, and support activities for delivery of integrated X ray and alpha particle spectrometer systems for lunar orbiter
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Logistics planning for phased programs
Logistics planning as integral part of phased program planning process, considering preliminary analysis, definition, design, development, fabrication, test and operations phases
Goodrum, J. C.↗
Design, development and fabrication of a Solar Experiment Alignment Sensor (SEAS)
The design, development and testing of a laboratory SEAS (Solar Experiment Alignment Sensor) system are presented. The system is capable of overcoming traditional alignment and calibration problems to permit pointing anywhere on the solar disc to an accuracy of five arc seconds. The concept, development and laboratory testing phases of the program are discussed, and particular attention has been given to specific problems associated with selection of materials, and components. The conclusions summarize performance capability and discuss areas for further study including the effects of solar limb darkening and effects of annual variations in the apparent solar diameter.
Bancroft, J. R.↗
Modular space station phase B extension program master plan
The project is defined for design, development, fabrication, test, and pre-mission and mission operations of a shuttle-launched modular space station. The project management approach is described in terms of organization, management requirements, work breakdown structure, schedule, time-phased logic, implementation plans, manpower, and funding. The programmatic and technical problems are identified.
Munsey, E. H.↗
Urine sampling and collection system
This specification defines the performance and design requirements for the urine sampling and collection system engineering model and establishes requirements for its design, development, and test. The model shall provide conceptual verification of a system applicable to manned space flight which will automatically provide for collection, volume sensing, and sampling of urine.
Fogal, G. L.↗
Study of solid rocket motors for a space shuttle booster. Appendix B: Prime item development specification
The specifications for the performance, design, development, and test requirements of the P2-156, S3-156, and S6-120 space shuttle booster solid rocket motors are presented. The applicable documents which form a part of the specifications are listed.
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Use of the space shuttle to avoid spacecraft anomalies
An existing data base covering 304 spacecraft of the U.S. space program was analyzed to determine the effect on individual spacecraft failures and other anomalies that the space shuttle might have had if it had been operational throughout the period covered by the data. By combining the results of this analysis, information on the prelaunch activities of selected spacecraft programs, and shuttle capabilities data, the potential impact of the space shuttle on future space programs was derived. The shuttle was found to be highly effective in the prevention or correction of spacecraft anomalies, with 887 of 1,230 anomalies analyzed being favorably impacted by full utilization of shuttle capabilities. The shuttle was also determined to have a far-reaching and favorable influence on the design, development, and test phases of future space programs. This is documented in 37 individual statements of impact.
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Design study of arresting gear system for recovery of space shuttle orbiters
A plan is reported for the design, manufacture, development, test, and production of an emergency arrestment system for the recovery of shuttle orbiters. Time and cost estimates are included. System testing and several optional test programs are discussed.
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Design and development of diborane shipping container
The design, development, and tests of a 200 pound container for the shipment of liquid diborane are reported. A record of the correspondence with the DOT to obtain a permit for liquid diborane shipment is presented.
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System safety plan for the ultraviolet spectrometer experiment S169
Comprehensive safety program requirements are defined and a methodology for implementing the defined safety tasks in support of the design, development, manufacturing, testing and flight phases of the ultraviolet spectrometer experiment is presented.
Heidelbach, R. G.↗
Study of airborne science experiment management concepts for application to space shuttle, volume 2
Airborne research management and shuttle sortie planning at the Ames Research Center are reported. Topics discussed include: basic criteria and procedures for the formulation and approval of airborne missions; ASO management structure and procedures; experiment design, development, and testing aircraft characteristics and experiment interfaces; information handling for airborne science missions; mission documentation requirements; and airborne science methods and shuttle sortie planning.
Mulholland, D. R.↗
Ice pack heat sink subsystem - phase 1, volume 2
The design, development, and test of a functional laboratory model ice pack heat sink subsystem are discussed. Operating instructions to include mechanical and electrical schematics, maintenance instructions, and equipment specifications are presented.
Roebelen, G. J., Jr.↗
Preliminary flight prototype potable water bactericide system
The development, design, and testing of a preliminary flight prototype potable water bactericide system are described. The system is an assembly of upgraded canisters composed of: (1) A biological filter; (2) an activated charcoal and ion exchange resin canister; (3) a silver chloride canister, (4) a deionizer, (5) a silver bromide canister with a partial bypass, and (6) mock-up instrumentation and circuitry. The system exhibited bactericidal activity against 10 to the 9th power Pseudomonas aeruginosa and/or Type IIIa, and reduced Bacillus subtilis by up to 5 orders of magnitude in 24 hours at ambient temperatures with a 1 ppm silver ion dose. Four efficacy tests were performed with a AgBr canister dosing anticipated fuel cell water. Tests show that a 0.05 ppm silver ion dose was bactericidal against 3 plus or minus 1 x 10 to the 9th power (5 plus or minus 1 x 10,000/ml Pseudomonas aeruginosa and/or Type IIIa in 15 minutes or less.
Jasionowski, W. J.↗