Follow on task - Optimized cost/performance design methodology Final report
Optimized cost and performance design of siamese booster/orbiter shuttle
Source record↗
SEARCH · Engineering Papers
Results for “tasks”
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Task 1.0 - Material and fabrication techniques
Antenna hardware elements for truss tubular strut construction
Source record↗
Master agreement task order 2 - Analyses and limited evaluations of payload and landing system structures for the survivable soft landing of instrument payloads
Computer programs for analysis and evaluation of payload and landing system structures for soft landing of instrument packages
Burton, D. J.↗
Comments on several reduced-gravity simulators used for studying lunar self-locomotive tasks
Subjective review of feel and operating characteristics of reduced-gravity simulators
Spady, A. A., Jr.↗
Apollo RCS Positive Expulsion Tankage Product Improvement Program. Task B - Long Term Compatibility Testing Final Report, Jul. 1967 - Sep. 1969
Useful operating life of Apollo and LM RCS propellant tank configurations
Source record↗
Investigation of the preparation of materials in space. Task 4 - Field management for weightless containerless processing Quarterly progress report, 22 Aug. - 31 Oct. 1969
Weightless containerless processing for space, electromagnetic position control, force measurements and techniques, and hydrodynamics
Frost, R. T.↗
Apollo communication systems support, task 5 - Lateral p-n-p design optimization Final report
Design optimization of lateral p-n-p transistors with minimum processing steps
Source record↗
Task 5 outgassing apparatus and gas analysis data, appendix I
Outgassing apparatus and gas analysis data for modular nuclear vehicle
Source record↗
Vacuum jacketed umbilical lines technology advancement study. Task 2 - Vacuum seal valves Final technical report
Vacuum jacketed components on launch umbilical tower service arms at Launch Complex 39 - vacuum seal valves
Martinez, J.↗
Vacuum jacketed umbilical lines technology advancement study. Task 4 - Rotary joint Final technical report
Vacuum jacketed components on launch umbilical tower service arms at Launch Complex 39 - low heat cryogenic rotary joint
Mursinna, R. C.↗
Vacuum jacketed umbilical lines technology advancement study. Task 5 - Vacuum probes Final technical report
Vacuum jacketed components on launch umbilical tower service arms at Launch Complex 39 - vacuum probes
Rewerts, G. R.↗
Vacuum jacketed umbilical lines technology advancement study. Task 6 - Central vacuum pulldown system Final technical report
Vacuum jacketed components on launch umbilical tower service arms at Launch Complex 39 - central vacuum pulldown system
Rewerts, G. R.↗
Vacuum jacketed umbilical lines technology advancement study. Task 7 - Bayonet joint Final technical report
Vacuum jacketed components on launch umbilical tower service arms at Launch Complex 39 - bayonet joints in cryogenic propellant and vent lines
Mursinna, R. C.↗
Research on display scanning, sampling, and reconstruction using separate main and secondary tracking tasks
Dynamic model for effects of random scanning and sampling on human operator tracking performance
Allen, R. W.↗
Investigation of the preparation of materials in space. Task 4 - Field management for positioning and processing of free suspended liquid materials Final report, 22 Aug. 1969 - 31 Apr. 1970
Melting and handling of molten material in weightless space environment
Frost, R. T.↗
Determination of processing and test facility requirements for large solid rocket motors. Volume 1 - Task 1 - Facility modification for full-length 260 inch diameter motor processing and test Final report
Facility modification plan for testing 260-inch diameter solid rocket engine
Lambert, W. L.↗
Determination of processing and test facility requirements for large solid rocket motors. Volume 2 - Task 2 - facility optimization Final report
Cost optimization for 260-inch diameter solid rocket engine test facility
Lambert, W. L.↗