NASA - National Aeronautics and Space Administration (NASA): Recent submissions
Now showing items 1921-1940 of 3613
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NACA-TN-3283
Abstract: The problem of determining the total forces, moments, and stability derivatives for a slender body performing slow maneuvers in a compressible fluid is treated within the assumptions of slender-body theory. General expressions ...Subject(s) : AERODYNAMIC , BODIES , COMPRESSIBLE , CROSS , DERIVATIVES , EQUATIONS , FLUIDS , FORCES , GEOMETRY , MANEUVERS , MOMENTS , MOTION , SECTIONS , SLENDER , STABILITY , -
NASA-CR-165720
Abstract: The properties were measured during static, slow rolling, and high-speed tests, and comparisons were made between data as acquired on indoor drum dynamometers and on an outdoor test track. In addition, mechanical properties ...Subject(s) : AIRCRAFT TIRES , DYNAMIC TESTS , MECHANICAL PROPERTIES , STATIC TESTS , -
NASA-LLIS-0537
Abstract: Description of Driving Event:
O-ring manufactured on MIDAS for vacuum seal was made with butt joint instead of 45° angle joint.Subject(s) : Parts Materials & Processes , -
NASA-LLIS-0295
Abstract: Description of Driving Event:
During the shuttle STS-4 mission, an orbiter (OV-102) hydraulic pump failed. A post flight examination discovered an aluminum particle wedged into one of the high pressure ...Subject(s) : Hardware , Industrial Operations , Parts Materials & Processes , -
NASA-LLIS-1237
Abstract: Description of Driving Event:
Current policy for classification of mishaps, and hence mishap investigation procedures is done by dollar value of loss or injury severity.Subject(s) : Administration/Organization , Aerospace Safety Advisory Panel , Policy & Planning , Risk Management/Assessment , Safety & Mission Assurance , -
NACA-RM-L8H12
Abstract: INTRODUCTION
Investigations of the lateral stability of sweepback wings have shown that except at low angels of attack, the lateral-stability parameters are primarily dependent on the stalling characteristics of the ... -
NASA-LLIS-0347
Abstract: Abstract:
When a contractor was absorbed by a second contractor early during the performance of the Mars Observer contract, the new contractor's management implemented methods that were not consistent ...Subject(s) : Administration/Organization , -
NASA-LLIS-2076
Abstract: Abstract:
In 2009, as construction of the International Space Station (ISS) approached completion, and the programs Multilateral Coordination Board (MCB) reflected on the process, they thought it would ...Subject(s) : Additional Categories.Flight Operations , Additional Categories.Ground Operations , Additional Categories.Hardware , Additional Categories.Payloads , Additional Categories.Program and Project Management , -
NASA-LLIS-1091
Abstract: Description of Driving Event:
During pre-operations for the 5A US Lab Closed Hatch Environmental Control & Life Support System/Thermal Control System (ECLSS/TCS) testing, a water separator fault occurred ...Subject(s) : Configuration Management , Flight Equipment , Flight Operations , Ground Equipment , Ground Operations , Hardware , Industrial Operations , Launch Process , Parts Materials & Processes , Policy & Planning , Range Operations , Research & Development , Risk Management/Assessment , Safety & Mission Assurance , Test & Verification , Test Article , Test Facility , -
NASA NPD 2081.1 REV A
Abstract: APPLICABILITY
This Directive is applicable to NASA Headquarters and NASA Centers, including Component Facilities. -
NASA-LLIS-3636
Abstract: The Microwave Scanning Beam Landing System (MSBLS) contract, originally controlled by Johnson Space Center (JSC), was split across NASA centers. The Kennedy Space Center (KSC) has operation and maintenance (O&M) responsibility ...Subject(s) : 0.Vehicle concepts , 1.Acquisition / procurement strategy and planning , 1.Engineering design and project processes and standards , 1.Ground Equipment , 1.Ground Operations , 1.Ground support systems , 1.Launch Systems , Center distribution of programs and management activities , Cross Agency coordination , -
NASA NPD 8900.1 REV G W/CHG 1
Abstract: APPLICABILITY
This NASA Policy Directive (NPD) applies to NASA Headquarters and Centers, including Component Facilities. -
NASA-LLIS-0717
Abstract: Practice:
The Fizeau interferometer is the most commonly used interferometer for testing optical components and systems used aboard spaceborne or space-related instrumentation. This guideline provides ... -
NACA-ARR-4B03
Abstract: INTRODUCTION
Several series of compression tests have been made on panels with Z-section stiffeners formed from flat sheet (see fig.1) to show the importance of relative dimensions in determining the strength of ...Subject(s) : ALCOA , ALLOY , ALLOYS , ALUMINUM , COMBINATIONS , COMPRESSIVE , COUNTRSUNK , RIVETS , SHEET , SHEETS , SKIN , STIFFENER , STRENGTH , STRESSED , -
NASA-TP-3110
Abstract: An experimental investigation was conducted to measure the forces, moments, and pressure distributions on the generic store separating from a rectangular box cavity contained in a flat plate surface at supersonic speeds. ...Subject(s) : CAVITIES , DISTRIBUTION , EXTERNAL , FLAT , FLOW , FREE , MACH , MEASUREMENT , MOMENTS , NUMBER , OILS , PHOTOGRAPHS , PLATES , PRESSURE , REYNOLDS , SEPARATION , SPEED , STORE , SUPERSONIC , VAPORS , -
NASA-LLIS-1509
Abstract: Abstract:
The Orbital Space Plane (OSP) Program started up the learning curve early by creating the Acquisition Management Office (AMO) specifically for developing the acquisition strategy, Request For ...Subject(s) : Procurement Small Business & Industrial Relations , -
NASA-TN-D-209
Abstract: An analysis has been made of results obtained in a systematic research program concerned with the effects of wing sweep, aspect ratio, taper ratio, and dihedral on the rolling moment due to sideslip of wing-fuselage ...Subject(s) : ASPECT , BODY , COMPRESSIBILITY , CONFIGURATIONS , GEOMETRY , MACH , MOMENTS , NUMBER , RATIO , ROLLING , SIDESLIP , SPEED , SUBSONIC , SWEPT , TESTS , TRANSONIC , TUNNEL , WIND , WING , WINGS , -
NASA-CR-2440
Abstract: Equations and tables are presented for the viscosity and thermal conductivity coefficients of gaseous and liquid oxygen at temperatures between 80 K and 400 K for pressures up to 200 atm. and at temperatures between 80 K ...Subject(s) : COEFFICIENTS , GASES , HIGH PRESSURE , LIQUIDS , OXYGEN , THERMAL CONDUCTIVITY , VISCOSITY , -
NACA-RM-A50C13
Abstract: INTRODUCTION
The location of air inlets on the sides of the fuselages of jet-propelled aircraft has received special emphasis recently because of the necessity of housing radar and armament in the fuselage noses, ... -
NASA-LLIS-0493
Abstract: Description of Driving Event:
A fatal accident involving the Ames/EFRF T-37B Jet Trainer (NASA 807) occurred east of California City, CA. at approximately 1:15 P.M. (PST) on November 8, 1982. NASA pilot ...Subject(s) : Aircraft , Human Factors , Safety & Mission Assurance ,

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