NASA - National Aeronautics and Space Administration (NASA): Recent submissions

Now showing items 2641-2660 of 3613

    • NASA-LLIS-0044 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1991
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      A painter in the utility annex stepped on a pipe, causing it to fracture at the interface of an attached valve. The pipe remained attached to the valve, but the leak sprayed ...
      Subject(s) : Emergency Preparedness , Facilities , Hardware , Industrial Operations ,

    • NASA-LLIS-0980 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2000
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      The Terra spacecraft relied on several state-of-the-art developments, as a result of the demanding resource requirements of the Terra instrument suite. These spacecraft ...
      Subject(s) : Ground Equipment , Test & Verification ,

    • NASA-LLIS-1445 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2003
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Abstract:
      Experience with PBMA indicates that a single configuration management/electronic library will not meet needs of all investigation participants.
      Subject(s) : Accident Investigation , Computers , Configuration Management , Information Technology/Systems , Policy & Planning , Procurement Small Business & Industrial Relations , Safety & Mission Assurance ,

    • NASA-LLIS-0590 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1998
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Abstract:
      Mars Pathfinder (MPF) flight software development departed from strict adherence to then existing institutional software standards in order to produce software that would contribute to lower ...
      Subject(s) : Concurrent Engineering , Cryogenic Systems , Industrial Operations , Occupational Health , Personal Protective Equipment , Rapid Prototyping , Software Life Cycle , System Architecture ,

    • NASA-LLIS-1432 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1989
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Abstract:
      Mishap while preparing to perform pneumatic flushing of debris from high pressure air lines in the 8- Foot High Temperature Tunnel (8'HTT).
      Subject(s) : Accident Investigation , Facilities , Hardware , Human Factors , Mishap Reporting , Safety & Mission Assurance ,

    • NASA-LLIS-0871 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2000
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      On January 4, 1995, at approximately 8:50 a.m., two technicians at WSTF were overcome and collapsed from breathing in an oxygen deficient atmosphere that formed during ...
      Subject(s) : Cryogenic Systems , Emergency Preparedness , Environment , Facilities , Ground Operations , Hazardous/Toxic Waste/Materials , Human Factors , Logistics , Packaging Handling Storage , Personal Protective Equipment , Policy & Planning , Risk Management/Assessment , Safety & Mission Assurance , Test Facility , Transportation ,

    • NASA-LLIS-0883 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2000
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Practice:
      Use of the Facility Chilled Water (FCW) System to provide the heat exchange medium for the hypergolic propellant Thermal Conditioning Units (TCU).

    • NACA-TN-1743 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1948
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Flight measurements have been made to determine the low-speed flying qualities of an airplane having a wing swept back 35° at the quarter-chord line. The lateral and detections stability and control characteristics ...
      Subject(s) : AIRPLANES , CHARACTERISTICS , CONTROL , DIHEDRAL , DIRECTIONAL , FLYING , LATERAL , LONGITUDINAL , QUALITIES , SIDESLIPPING , SLOTS , STABILITY , STALLING , STATIC , SWEPTBACK , WING , WINGS ,

    • NACA-TM-X-1665 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1968
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Sideslip angle effects on static stability characteristics of T tail transport configuration
      Subject(s) : AERODYNAMIC , AIRCRAFT , ANGLE , ATTACK , CHARACTERISTICS , COEFFICIENTS , CONFIGURATIONS , MOMENTS , SIDESLIP , STABILITY , STATIC , SURFACES , TAIL , TRANSPORT , YAWING ,

    • NASA-LLIS-2737 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2010
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Abstract:
      While radio frequency (RF) Shuttle Main Engine telemetry data was being recorded during the vehicle ascent phase of STS-123, off-nominal noise in the data stream, combined with the use of a ...
      Subject(s) : Configuration control and data management , Crew Survival Systems , Engineering design and project processes and standards , Ground Equipment , Ground Operations , Ground support systems , Human factors impact on mission design , Launch support systems , Security , Software , Test & Verification ,

    • NASA-LLIS-0164 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1992
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      Non-collapsible handrails are in place on the OPF buckets. When the OPF bucket (platform) is raised to the full up position, the hand rails stress, creating the potential ...
      Subject(s) : Facilities , Ground Operations ,

    • NACA-TM-798 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1936
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Investigations on the flow phenomena at plates and cambered models were carried out with the aid of force measurements, some pressure distribution measurements, and photographic observation. The experimental methods are ...

    • NASA-LLIS-1187 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1992
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      At the Kennedy Space Center on August 11, 1992, in Vehicle Assembly Building (VAB) High Bay #1, the 250 Ton crane #1 was stacking the left forward Solid Rocket Motor (SRM) ...
      Subject(s) : Facilities , Ground Equipment , Ground Operations , Hardware , Human Factors , Industrial Operations , Launch Process , Lifting Devices , Mishap Reporting , Packaging Handling Storage ,

    • NACA-TN-2445 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1951
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Results are presented of wind-tunnel tests made at low speed of various small-scale models of sweptback, sweptforward, and yawed wings. The tests covered changes in aspect ratio, taper ratio, and tip shape. Some data were ...
      Subject(s) : COMPLETE , DESIGN , DEVICES , HIGH , LIFT , SWEEP , VARIABLES , WINGS ,

    • NASA-LLIS-0836 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2000
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Practice:
      Engage in refurbishment activities to rebuild and prepare for reuse of the Solid Rocket Boosters (SRB's) after each Space Shuttle Orbiter launch. These refurbishment activities include: (1) ...

    • NACA-TR-400 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1932
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Aerodynamic force tests on a slotted Clark Y wing were conducted in a vertical wind tunnel to determine the best position for a given auxiliary airfoil with respect to the main wing. A systematic series of 100 changes in ...
      Subject(s) : AERODYNAMIC , AIRFOILS , ANGLE , ATTACK , COEFFICIENTS , GEOMETRY , LIFT , LOCATION , POSITION , PREVENTION , SLOTS , STALLING , TESTS , TUNNEL , WIND , WING , WINGS ,

    • NASA-LLIS-0015 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1993
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      Hydraulic fluid leakage was noted at the interface of the flex hose and Rosan fitting on a hydraulic pump. The fittings were a different size at each end of the flex hose. ...
      Subject(s) : Facilities , Fire Protection , Ground Operations , Hardware , Industrial Operations , Parts Materials & Processes , Spacecraft ,

    • NASA-LLIS-0948 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1995
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      The Challenger (Space Shuttle Flight #51L) accident triggered a detailed review of all of the joints in the Solid Rocket Motor. Analyses showed a potential weakness and ...
      Subject(s) : Energetic Materials - Explosive/Propellant/Pyrotechnic , Launch Vehicle ,

    • NACA-TN-4405 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1958
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: A free-flight investigation was conducted between Mach numbers of 0.75 and 1.35 to determine the effects on model total drag and pressure drag of (a) canopy location (along a parabolic body of revolution), (b) canopy ...

    • NASA-CR-1536 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1970
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Effects of surrounding structure on sonic fatigue.
      Subject(s) : ACOUSTIC MEASUREMENT , FATIGUE TESTS , S-N DIAGRAMS , STRESS ANALYSIS , TRANSONIC FLOW ,