NASA - National Aeronautics and Space Administration (NASA): Recent submissions
Now showing items 3381-3400 of 3613
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NACA-RM-A51D27
Abstract: INTRODUCTION
Theoretical studies and a number of experimental investigations have indicated that camber and twist may improve the characteristics h. of swept wings. This improvement results from more ... -
NASA-LLIS-4516
Abstract: Abstract:
Configuration and Data Management (CDM) is performed at the Kennedy Space Center (KSC) for hardware and software by the different programs and projects independently of the Center/Institution. ...Subject(s) : Business Processes , Configuration and Data Management , Cross Agency Coordination , Information System , Organization Planning , -
NASA-LLIS-0419
Abstract: Abstract:
The SEASAT-A Synthetic Aperture Radar system end-to-end gain was instable due RF leakage that varied with the sensor gain state and with temperature. Use of prototype models and diagnostic ...Subject(s) : Communication Link , Design Verification , Hardware , Spacecraft Radar , Test & Verification , -
NASA-TN-D-6243
Abstract: Predicting aerodynamic characteristics of arrow, delta, and diamond wing platforms using Prandtl-Glauert transformationSubject(s) : AERODYNAMIC , ARROW , CHARACTERISTICS , CHARTS , COMPRESSIBLE , DELTA , FLOW , GRAPHS , MATHEMATICS , PLANFORMS , SUBSONIC , TRANSFORMATIONS , VORTICES , WING , WINGS , -
NASA-LLIS-0214
Abstract: Description of Driving Event:
Criteria for design, performance, launch commit, and other operations have used "ambient" conditions as a reference or base for evaluating systems which could be affected ...Subject(s) : Environment , -
NASA-LLIS-1239
Abstract: Description of Driving Event:
Potential slide or cancellation of Cockpit Avionics Upgrade for the Orbiter.Subject(s) : Aerospace Safety Advisory Panel , Computers , Configuration Management , Flight Operations , Human Factors , Risk Management/Assessment , Safety & Mission Assurance , Software , Spacecraft , -
NACA-RM-L50A04
Abstract: INTRODUCTION
An investigation is being conducted on a 47.7° sweptback wing with aspect ratios 5.1 and 6.0 to provide low-speed large-scale data on relatively high-aspect-ratio sweptback wings. In order to indicate ... -
NASA-LLIS-1084
Abstract: Abstract:
The primary cause of this Central Power Plant (CPP) pressurized steam line incident was that no one took responsibility for coordinating all aspects of executing the outage.
Recommendations ...Subject(s) : Communication Systems , Facilities , Human Factors , Industrial Operations , Logistics , Mishap Reporting , Occupational Health , Packaging Handling Storage , Pressure Vessels , Safety & Mission Assurance , -
NASA-TN-D-4759
Abstract: Noncavitating and cavitating performance of two low area ratio water jet pumps with throat lengths of 5.66 diameters.Subject(s) : CAVITATION FLOW , HYDRAULIC JETS , JET PUMPS , NOZZLE GEOMETRY , PERFORMANCE PREDICTION , PERFORMANCE TESTS , RATIOS , THROATS , -
NACA-TM-838
Abstract: The monocoque form of airplane construction has introduced a number of new problems to the stress calculator and the designer. The problems for the stress calculator fall into two groups: the determination of the stress ... -
NASA-LLIS-0077
Abstract: Description of Driving Event:
While pressurizing the oxidizer propellant tank, a change in ullage pressure of 8 psi occurred and caused the computer program to indicate that the interface and supply ...Subject(s) : Energetic Materials - Explosive/Propellant/Pyrotechnic , Pressure Vessels , Software , -
NASA-LLIS-1008
Abstract: Description of Driving Event:
Environmental Regulations Resulting in Manufacturing Process and Test Certification Changes for RSRM.Subject(s) : Aerospace Safety Advisory Panel , Energy , Environment , Ground Operations , Hazardous/Toxic Waste/Materials , Policy & Planning , Safety & Mission Assurance , Test & Verification , -
NACA-TN-2699
Abstract: On the basis of linearized supersonic-flow theory the stability derivatives Cma and Cmq (moment coefficients due to angle of attack and steady pitching velocity, respectively) and CLq (lift ... -
NASA-LLIS-0636
Abstract: Description of Driving Event:
On 7/12/99, a mechanic was performing a verification leak test (using a 2900 psig gaseous nitrogen pressure source) of a 1/2" hand valve when an incorrect fitting blew ...Subject(s) : Energetic Materials - Explosive/Propellant/Pyrotechnic , Ground Equipment , Pressure Vessels , Test & Verification , Test Facility , -
NASA NPR 8910.1 REV C W/CHG 1
Abstract: PURPOSE
This NPR delineates the responsibilities and implementing requirements for the Agency's use of animals in research, testing, teaching, and hardware development activities, including such ... -
NASA-LLIS-1399
Abstract: Abstract:
All projects involving multiple Centers require diplomacy and sensitivity to human relations in order to overcome Center-to-Center issues that may otherwise undermine the projects' success.Subject(s) : Administration/Organization , communication , competition , conflict , External Relations , multiple centers , Policy & Planning , Program and Project Management , Risk Management/Assessment , -
NASA-LLIS-0867
Abstract: Practice:
GN2 is provided to the actuator breather of pneumatically actuated valves used in hostile environments (salt spray, high humidity, SRB exhaust). -
NACA-RM-A54H27
Abstract: INTRODUCTION
The target-pursuit maneuvers or programmed trajectory of guided missiles frequently require flight at large angles of attack (of the order of 30°), particularly at high altitudes. Limited experimental ...Subject(s) : AERODYNAMIC , ANGLE , ATTACK , CHARACTERISTICS , CONFIGURATIONS , CRUCIFORM , LONGITUDINAL , MACH , MISSILE , NUMBER , STABILITY , TESTS , TUNNEL , WIND , WINGS , -
NASA-LLIS-5936
Abstract: At approximately 9:00 p.m., on 28 January 2010, a six-inch diameter fire suppression (Firex) main supply pipe coupling separated from a pipe elbow releasing approximately 29,000 gallons of water into the Kennedy Space ...Subject(s) : Additional Categories.Accident Investigation , Additional Categories.Facilities , Additional Categories.Fire Protection , Safety and Mission Assurance.Maintenance , -
NASA-LLIS-0391
Abstract: Abstract:
The Galileo mission twice experienced difficulties with recovery from safing errors due to a lack of a formal safing recovery plan and to software/documentation that had not been kept current ...Subject(s) : Commanding , Configuration Management , Software , Spacecraft ,

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