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

Now showing items 2541-2560 of 3613

    • NACA-TR-679 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1939
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: A test installation was used in which an airfoil of 7-foot span was mounted vertically between the upper and the lower sides of the closed test section so that two-dimensional flow was approximated.
      Subject(s) : AERODYNAMIC , AIRFOIL , AIRFOILS , CHARACTERISTICS , COEFFICIENTS , DEVICES , DIMENSIONAL , DRAG , FLAPS , FLOW , LIFT , LOCATION , MOMENTS , PITCHING , POSITION , PROFILES , SLOTS , SPLIT , TESTS , TUNNEL , TWO , WIND , WING ,

    • NASA-LLIS-1626 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2005
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Abstract:
      On the afternoon of June 17, 2004, there was a request to implement an approved Configuration Change Request to increase the left wing-fuselage clearance of the X-43A research vehicle. To ...
      Subject(s) : Accident Investigation , Aircraft , Extra-Vehicular Activity , Ground Operations , Human Factors , Research & Development , Test Article ,

    • NACA-WR-L-261 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1942
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: An investigation was made in the 7- by 10-foot wind tunnel of an NACA 23012 airfoil equipped with a Handley Page slat and a slotted and a split flap. The purpose of the investigation was to determine the aerodynamic section ...
      Subject(s) : AIRFOILS , CHAR , FLAPS , HANDLEY , MOMENTS , NACA , ORDINATES , SLATS , SLOTS , SLOTTED , SPLIT , WING ,

    • NASA-TM-X-62197 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1973
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: An investigation has been conducted to determine the aerodynamic characteristics of a large-scale subsonic jet transport model with an externally blown triple-slotted flap. The lift of the model was augmented by the turbofan ...
      Subject(s) : AERODYNAMIC , AIRCRAFT , AUGMENTATION , BLOWN , CHARACTERISTICS , CONTROL , EXTERNALLY , FLAPS , JET , LATERAL , LIFT , LONGITUDINAL , SWEPT , TESTS , TRANSPORT , TUNNEL , WIND , WINGS ,

    • NASA-LLIS-0895 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2000
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      I was involved in a project in which we were developing a new control and data acquisition system for an instrument to be used to measure radiation absorption in clouds. ...
      Subject(s) : Computer-Aided Design/Manufacturing/Engineering , Computers , Flight Equipment , Hardware , Information Technology/Systems , Risk Management/Assessment , Software , Test & Verification ,

    • NACA-TN-3501 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1955
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: An investigation to determine the aerodynamic characteristics of a series of thin, rectangular wings was conducted in the Ames 16-foot high-speed wind tunnel, utilizing the transonic bump technique over a mach number range ...

    • NASA-SP-164 VOL 2 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1969
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Thermal radiation exchange between surfaces and enclosures.
      Subject(s) : BLACK BODY RADIATION , ENCLOSURES , MONTE CARLO METHOD , RADIATIVE HEAT TRANSFER , SURFACE REACTIONS , THERMAL RADIATION ,

    • NASA-LLIS-4417 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2011
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: During the Space Shuttle STS-80 mission, the two planned Extravehicular Activities (EVA) were scrubbed when the astronauts discovered that the outer airlock hatch would not open. This impacted the plan to evaluate the EVA ...
      Subject(s) : Engineering design and project processes and standards , Lander Systems , Launch Systems , Level II/III requirements definition , Logistics and maintenance ,

    • NASA-LLIS-4896 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2012
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Performing an independent/integrated logistics assessment is a good tool to assess the progress of logistics support planning and analyses. The assessment identifies weaknesses and gaps in the support planning. It is ...

    • NASA-LLIS-0513 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1994
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Subject(s) : Environment , Hardware ,

    • NASA-LLIS-1342 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2003
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      Due to three major factors the Project's budget was not sufficient to meet its primary objectives. One, the Project was the most significant and often times only customer ...
      Subject(s) : Logistics , Policy & Planning , Risk Management/Assessment ,

    • NACA-RM-L8G05 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1948
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: INTRODUCTION
      A wing having triangular plan form, 60° of sweepback at the leading edge, and 10-percent-tuck biconvex airfoil sections has been tested in the Langley full-scale tunnel as part of a general investigation ...

    • NACA-TN-1813 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1949
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: A study of experimental pressure distributions and sections was made. A correlation appears to exist between the drag-divergence Mach number and the free-stream Mach number and the free-stream Mach number for which sonic ...

    • NASA-LLIS-2776 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2010
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Abstract:
      The Logistics organization treats parts as parts only, with no provisions for storing related parts as kits. Because of the nature of the Thermal Control System (TCS) blankets and supports, ...
      Subject(s) : & Processes , Configuration control and data management , Configuration Management , Ground Operations , Ground processing and manifesting , Handling , Logistics , Materials , Mishap Reporting , NASA Standards , Occupational Health , Packaging , Parts , Payloads , Personal Protective Equipment , Policy & Planning , Pressure Vessels , Procurement , Program and Project Management , Range Operations , Research & Development , Risk Management/Assessment , Safety & Mission Assurance , Security , Small Business & Industrial Relations , Software , Spacecraft , Standard , Storage , Test & Verification , Test Article , Test Facility , Training Equipment , Transportation ,

    • NASA-LLIS-0364 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1994
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Abstract:
      Galileo design optimizations over the years exacerbated interactions between spacecraft power and the propellant tanks. During the cruise phase, high power and heat dissipation near the ...
      Subject(s) : Configuration Management , Test & Verification ,

    • NASA-LLIS-0111 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1992
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      Quick disconnects, utilized for providing gasses to the space shuttle main engine drying/purge lines and the main propulsion system LH2 prepressurization system are identical ...
      Subject(s) : Facilities , Ground Equipment , Ground Operations , Human Factors , Launch Process , Launch Vehicle ,

    • NASA-LLIS-1107 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1999
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      Initial Operational Capability of Crew Return Vehicle (CRV).
      Subject(s) : Aerospace Safety Advisory Panel , Flight Operations , Policy & Planning , Spacecraft ,

    • NASA-LLIS-2419 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2009
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Abstract:
      The Aquarius reflector was damaged by over-testing during a 2007 test in the JPL acoustic test chamber. The root cause was attributed to a procedural deviation, and the proximate cause was ...
      Subject(s) : Additional Categories. , Additional Categories.Facilities , Additional Categories.Flight Equipment , Additional Categories.Ground Equipment , Additional Categories.Hardware , Additional Categories.Mishap Reporting , Additional Categories.Payloads , Additional Categories.Spacecraft , Additional Categories.Test Article , Additional Categories.Test Facility , Engineering Design (Phase C/D). , Engineering Design (Phase C/D).Spacecraft and Spacecraft Instruments , Integration and Testing , Program Management. , Program Management.Communications between different offices and contractor personnel , Program Management.Contractor relationships , Safety and Mission Assurance. , Safety and Mission Assurance.Quality ,

    • NASA-LLIS-0731 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2000
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Practice:
      Use a standard SDS in spacecraft where possible which utilizes a standard data bus and space flight qualified versions of widely used hardware and operating software systems.

    • NACA-TR-578 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1937
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: The dynamic longitudinal stability characteristics of eight airplanes as defined by the period and damping of the longitudinal oscillations were measured in flight to determine the degree of stability that may be expected ...