Stage sizing data for an unmanned planetary sample return mission, task E-94 Project technical report
Outbound and inbound stage weight requirements for planetary sample return mission payload and energy requirements - graphs
Gilbertson, R. D.↗
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Results for “tasking”
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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Gyro bearing improvement program, tasks 1 to 6 Final report
Surface evaluation of stainless steel gyro bearings manufactured by various hardening techniques
Allen, S.↗
Task 4 stage data and performance report for casing treatment investigations. Evaluation of range and distortion tolerance for high Mach number transonic fan stages, volume 1
Test description and results for high Mach number transonic fan stages to determine range and distortion tolerance for various rotor tip casing treatment configurations
Tesch, W. A.↗
Task 4 stage data and performance report for casing treatment investigations. Evaluation of range and distortion tolerance for high Mach number transonic fan stages, volume 2
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
Tesch, W. A.↗
Housekeeping concepts for manned space systems data book. Volume 1 - Waste control tasks and system concepts /DRL line item no. 4/
Handling of waste products on spacecraft to include identification, potential for on-board utilization, pretreatment requirements for storage, and disposal concepts - Vol.1
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Demonstration of the range over which the Langley Research Center digital computer charring ablation program /CHAP/ can be used with confidence. Task 1 - Collection of properties data and ablation test data for three charring materials, and results of qualifying calculations with CHAP Final report
Thermochemical and thermophysical properties and ablation test data for three charring ablators
Green, K. A.↗
Design and development of a thirty watt per pound 250 square rollup subsolar array. Additional tasks - Stowed blanket dynamics, in-plane structural characteristics
Effects of warp tension on stowed blanket dynamics and in-plane structural characteristics of rollup solar arrays
Hanson, K.↗
An engineering study of onboard checkout techniques. Task 1: Requirements analysis and concepts
Concepts and requirements analysis for automated onboard checkout of manned space station
Mckinley, A. P.↗
An engineering study of onboard checkout techniques. Task 2: Software
Language and executive software requirements for automated onboard checkout of manned space station
Welsh, D. M.↗
An engineering study of onboard checkout techniques. Task 3: Onboard maintenance
Technology for implementation of onboard electronics maintenance facility for manned space station
Beck, R. P.↗
An engineering study of onboard checkout techniques. Task 5: Subsystem level failure modes and effects
Failure effects analysis of guidance, navigation, and control, data management, and communications subsystems
Frizzell, J. H.↗
Development of seal ring carbon-graphite materials (tasks 3 and 4)
Thermal, chemical, and wear properties of carbon-graphite seal ring materials at air temperature to 1300 F
Fechter, N. J.↗
Spaceborne computer multi-element system configuration architecture refinement, task 1 report
Architectural design of spaceborne computer system operating in multi-element configuration
Kennedy, J. R., Sr.↗
Influence of vestibular stimulation and display luminance on the performance of a compensatory tracking task
Vestibular nystagmus and display luminance effects on hand-eye coordination in compensatory tracking of aircraft instrument
Benson, A. J.↗
OSSA's R and D tasks toward seventies stress satellites for serving man
Ossa R and D program noting budget allocations, satellite programs and international projects
Naugle, J. E.↗
Biowaste resistojet propellant system, biological and functional analysis, task 1 and 2
The influence of chemical contaminants in potential biowaste sources upon the design and interface requirements of a biowaste resistojet propulsion system for a space station and/or base are evaluated. Chemical contaminants are defined as all compounds present in biowaste other than carbon dioxide, water, and methane. The latter are the nominal effluent candidates for the biowaste resistojet.
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Remote detection of trailing vortices, task 3, modification 3
The operation of a frequency tracker for use with the laser Doppler velocimeter (LDV) is reported. Topics discussed include: laser beam profile, lens matching, and LDV resolution data. It is concluded that the LDV provides good ground wind signals. The loss in sensitivity of the cavity system at high frequencies is partly compensated by an increase in the scattering cross section of the atmosphere due to dust.
Fridman, J.↗
Experiment module concepts study. Volume 5 book 1, appendix A: Shuttle only task
Results of a preliminary investigation of the effect on the candidate experiment program implementation of experiment module operations in the absence of an orbiting space station and with the availability of the space shuttle orbiter vehicle only are presented. The fundamental hardware elements for shuttle-only operation of the program are: (1) integrated common experiment modules CM-1, CM-3, and CM-4, together with the propulsion slice; (2) support modules capable of supplying on-orbit crew life support, power, data management, and other services normally provided by a space station; (3) dormancy kits to enable normally attached modules to remain in orbit while shuttle returns to earth; and (4) shuttle orbiter. Preliminary cost estimates for 30 day on-orbit and 5 day on-orbit capabilities for a four year implementation period are $4.2 billion and $2.1 billion, respectively.
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