NASA - National Aeronautics and Space Administration (NASA): Recent submissions
Now showing items 1081-1100 of 3613
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NASA-LLIS-0326
Abstract: Description of Driving Event:
Spacelab did not have standard utility interfaces at each rack, thus each experimenter or the integration organization had to provide design and routing for each required ...Subject(s) : Flight Equipment , Hardware , Logistics , Payloads , Spacecraft , -
NASA-TN-D-552
Abstract: A series of unbraked (freely rolling) taxi tests were conducted at the Langley landing-loads track with a 32 x 8.8, type 7, 22-ply-rating ribbed-tread aircraft tire to obtain data on tire retardation forces developed during ...Subject(s) : ACCELERATION (PHYSICS) , AERODYNAMIC COEFFICIENTS , AERODYNAMIC DRAG , AIRCRAFT TIRES , JET AIRCRAFT , RETARDING , RUNWAYS , SLUSH , TAKEOFF , WATER , -
NASA-LLIS-5477
Abstract: When fuel cell power plants (FCPs) were developed for the Space Shuttle, KSC had minimal capability to repair them. As a result, even FCPs needing only minor repairs had to be returned to the vendor for repair. In the ...Subject(s) : Acquisition / procurement strategy and planning , Cryogenic Systems , Engineering design and project processes and standards , Ground processing and manifesting , Ground support systems , Human factors planning , Launch Vehicle , Parts , Materials , & Processes , Power , Requirements critical to costing and cost credibility , -
NASA-LLIS-1060
Abstract: Description of Driving Event:
International Space Station (ISS) Computer Hardware Upgrades.Subject(s) : Aerospace Safety Advisory Panel , Hardware , Information Technology/Systems , Policy & Planning , Research & Development , Risk Management/Assessment , Safety & Mission Assurance , Software , Spacecraft , Test & Verification , -
NACA-RM-A7I30
Abstract: INTRODUCTION
For the development of a satisfactory air-induction system of an aircraft, several aerodynamic criteria must be evaluated in conjunction with those involving structural design and installation. ... -
NASA-LLIS-0674
Abstract: Practice:
Well made, clamped, and temperature stabilized circular O-rings should be used in the design of reliable, reusable and long life seals in vacuum sealing applications. -
NASA-LLIS-1716
Abstract: Abstract:
Power cables in tight power cabinets are susceptible to damage from penetrating fasteners.Subject(s) : Additional Categories. , Additional Categories.Configuration Management , Additional Categories.Energy , Additional Categories.Facilities , Additional Categories.Personal Protective Equipment , Additional Categories.Risk Management/Assessment , Engineering Design (Phase C/D). , Engineering Design (Phase C/D).Power , Manufacturing and Assembly , Safety and Mission Assurance. , Safety and Mission Assurance.Maintenance , Safety and Mission Assurance.Quality , -
NASA-LLIS-1486
Abstract: Abstract:
Formal, archival documentation of the original investigation and the subsequent tests and analyses conducted to resolve the problem of the cracks found in the flowliners at the gimbal joint ...Subject(s) : Program and Project Management , -
NASA NPR 9260.1
Abstract: PURPOSE
This NASA Procedural Requirements (NPR) document provides the financial management requirements for handling the accounting for NASA Unfunded Liabilities, Unearned Revenues, Other Liabilities, ... -
NASA NPR 3335.1 REV H
Abstract: Purpose
a. NASA's Competitive Placement Plan
(1) This NPR provides the procedures and requirements of NASA's Competitive Placement Plan. This NPR shall be used in conjunction with ... -
NACA-RM-L8D06
Abstract: INTRODUCTION
As a part of the general investigation of the landing characteristics of wings for transonic and supersonic airplanes, tests have been made in the Langley full-scale tunnel to determine the aerodynamic ... -
NASA-STD-8739.1 REV A W/CHG 2
Abstract: This standard prescribes NASA's technical requirements, procedures, and documentation requirements for polymeric applications for electrical and electronic assemblies.
Purpose
This publication sets ... -
NASA-LLIS-0439
Abstract: Abstract:
A rotating prism motor aboard the TOPEX spacecraft experienced a sudden in-flight failure due to the use of perfluoropolyalkyether (PFPE) based lubricant on titanium bearings. Pure titanium ...Subject(s) : Hardware , Parts Materials & Processes , -
NACA-TN-1291
Abstract: INTRODUCTION
In order to provide fundamental design data the National Advisory Committee for Aeronautics has undertaken the expedient of publishing collections of data obtained in specific investigations and, whenever ...Subject(s) : AIRFOILS , CHAR , CLARK , ELEVATORS , END , HINGE , HORIZONTAL , LIFT , LIFTING , MOMENTS , NACA , ORDINATES , ORDINATS , PLATES , SURFACE , SURFACES , TAIL , THEORIES , -
NASA-TN-D-7099
Abstract: An investigation has been conducted to determine the effects of wing camber and twist on the longitudinal aerodynamic characteristics of a wingbody configuration. Three wings were used each having the same planform (aspect ...Subject(s) : AERODYNAMIC , AIRCRAFT , CAMBER , COEFFICIENTS , CONFIGURATIONS , PERFORMANCE , PLANFORMS , SPEED , STABILITY , SUBSONIC , SWEPTBACK , WING , WINGS , -
NASA-LLIS-1256
Abstract: Description of Driving Event:
Prior to selecting a project to be funded, we rank each project against an AHP model that was based on the values of the program. We placed a 5 maximum user limitation on ...Subject(s) : Software , -
NACA-RM-L52C11
Abstract: INTRODUCTION
As part of a broad program to investigate the low-speed aerodynamic characteristics of sweptback wings, the static longitudinal stability characteristics of a 450 sweptback wing of aspect ratio ... -
NASA-TN-D-8151
Abstract: The fundamentals of fluid sealing, including seal operating regimes, are discussed and the general fluid-flow equations for fluid sealing are developed. Seal performance parameters such as leakage and power loss are ...Subject(s) : BOUNDARY LAYERS , FLUIDS , FRICTION , LAMINAR FLOW , LEAKAGE , LUBRICATION , PERFORMANCE , SEALS (STOPPERS) , SURFACE DISTORTION , TURBULENT FLOW , WEAR , -
NASA-LLIS-1071
Abstract: Description of Driving Event:
Effects of Radiation Exposure on ISS Expedition Crews.Subject(s) : Aerospace Safety Advisory Panel , Flight Operations , Medical , Occupational Health , Risk Management/Assessment , Safety & Mission Assurance , -
NASA NPR 8530.1 REV A
Abstract: PURPOSE
Consistent with responsible environmental stewardship as defined in the NASA 2003 Strategic Plan, NASA's Environmental Management Policy Directive (NPD) 8500.1, and consistent with the requirements ...

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