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

Now showing items 2601-2620 of 3613

    • NASA NPR 4200.1 REV G 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2010
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Purpose
      a. This NASA Procedural Requirements (NPR) 4200.1, NASA Equipment Management Procedural Requirements, supports the policy outlined in the NASA Policy Directive (NPD) 4200.1, Equipment Management. ...

    • NASA-LLIS-0435 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1996
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Abstract:
      A SEASAT-A subassembly was damaged during thermal-vacuum test due to the configuration of GSE test equipment. A reed relay in a commercial data scanner was connected to circuits requiring +5 ...
      Subject(s) : Configuration Management , Energy , Flight Equipment , Ground Equipment , GSE Interface FMECA , Hardware ,

    • NASA-LLIS-0235 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1993
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      A wind turbine was lowered from its tower and secured to a ground level assembly stand. A blade tip was then removed and the work crew broke for lunch. After lunch the ...
      Subject(s) : Industrial Operations , Lifting Devices ,

    • NACA-TN-1270 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1947
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: The aerodynamic characteristics of seven unswept tapered wings were determined by calculation from two-dimensional data and by wind-tunnel tests in order to demonstrate the accuracy of the calculations and to show some of ...
      Subject(s) : AIRFOIL , AIRFOILS , ASPECT , CHARACTERISTICS , LARGE , MOMENTS , NACA , PITCHIN , PRESSURE , RATIO , ROUGHNESS , SERIES , STALLING , SURFACES , TAPERED , TESTS , TUNNEL , WIND , WINGS ,

    • NASA-TN-D-6575 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1971
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: A summary was made of all NASA (and NACA) research and experience related to the spin and recovery characteristics of light personal-owner-type general-aviation airplanes. Very little of the research deals with light ...

    • NASA-LLIS-1252 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1998
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      Since the award of the Basic Space Station Contract numerous changes have been authorized, but there was no consistent, established method of authorizing and notifying the ...
      Subject(s) : Administration/Organization , Configuration Management , Independent Verification and Validation , Policy & Planning , Procurement Small Business & Industrial Relations , Risk Management/Assessment , Safety & Mission Assurance , Test & Verification ,

    • NACA-RM-L51L10 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1952
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: INTRODUCTION
      The spoiler used as a lateral-control device has been the subject of considerable investigation at low and high speeds, and on both swept and unswept wings (references 1 to 7). Many of the advantages ...

    • NASA-TN-D-7351 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1973
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: An investigation was conducted at the Langley aircraft landing loads and traction facility to determine the cornering characteristics of a 40 x 14-16 type VII aircraft tire. These characteristics, which include the ...
      Subject(s) : AIRCRAFT TIRES , COEFFICIENT OF FRICTION , CONTACT RESISTANCE , DATA ACQUISITION , EQUIPMENT SPECIFICATIONS , PERFORMANCE TESTS , SURFACE PROPERTIES ,

    • NASA-LLIS-0099 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1992
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      An APU hydrazine isolation valve assembly was removed and sent to the shipping section of logistics without being properly packaged for safe handling. In addition, there ...
      Subject(s) : Energetic Materials - Explosive/Propellant/Pyrotechnic , Hardware , Hazardous/Toxic Waste/Materials , Packaging Handling Storage ,

    • NASA-LLIS-1068 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1999
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      Shuttle Spares Support Will Likely Decline With an Increased Flight Rate.
      Subject(s) : Aerospace Safety Advisory Panel , Financial Management , Logistics , Parts Materials & Processes , Policy & Planning , Risk Management/Assessment , Spacecraft ,

    • NASA-LLIS-0655 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2000
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Practice:
      Conduct a formal Preliminary Design Review (PDR) at the system and subsystem levels prior to the start of subsystem detail design, to assure that the proposed design and associated implementation ...

    • NASA-LLIS-1561 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2005
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Abstract:
      A. Reviews: General feedback received from all levels of project participants There are too many reviews without clear definition of their purpose. As a result, reviews tended to overlap in ...
      Subject(s) : AATT , Budget , General Feedback , Independent Verification and Validation , Policy & Planning , Program and Project Management , Reporting , Reviews , Schedule , Technical Publications ,

    • NASA-LLIS-1422 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2004
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Abstract:
      Ensuring that a Project's collective wisdom is collected, archived, and disseminated depends on including a schedule, budget, and process for their accomplishment in the Project plan.
      Subject(s) : knowledge capture , knowledge dissemination , Project closeout , Risk Management/Assessment , Safety & Mission Assurance ,

    • NACA-RM-L7E13 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1947
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Wind-tunnel investigations were made in pitch and yaw with and without split flaps. Presence of the fuselage had negligible effect on values of maximum lift coefficient and slope of lift curve, but caused a destabilizing ...
      Subject(s) : FLAPPING , FLAPS , FUSELAGES , SPLIT , WINGS ,

    • NASA-LLIS-0410 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1996
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Abstract:
      Mutual interference among the two Viking Orbiters and the two Viking Landers caused a loss of downlink carrier lock and telemetry data several times during the Viking extended mission. The ...
      Subject(s) : Communication Systems , Flight Equipment , Ground Equipment , Multiple Mission Planning , Spacecraft ,

    • NASA-LLIS-0207 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1992
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      A very disorganized system of making, archiving, and reporting natural environmental conditions at KSC has evolved. Several organizations make measurements and archive ...
      Subject(s) : Administration/Organization , Environment , Launch Process ,

    • NACA-TN-808 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1941
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: An investigation was made in the NACA 7- by 10-foot wind tunnel to determine the effect of slot-lip location on the aerodynamic section characteristics of an NACA 23012 airfoil with a 30-percent-chord slotted flap. Tests ...
      Subject(s) : AIRFOILS , CHAR , CHORD , DEVICES , EXTENDED , FLAPS , FOWLER , FULL , HIGH , LIFT , LIP , LMAL , MOMENTS , NACA , ORDINATES , SLOTTED , WING , WINGS ,

    • NASA NPR 1387.1 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2010
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Purpose
      This NPR provides responsibilities, procedures, and requirements for the conduct of the NASA Exhibit Program.
      Applicability
      This NPR applies to NASA Headquarters and ...

    • NASA-LLIS-1230 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1999
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      During dimensional inspection of orbital tube welds involving 316L tubing, it was found that 8 of 8 welds failed because of weld mismatch. The weld joints were located ...
      Subject(s) : Hardware , Industrial Operations , NASA Standards , Parts Materials & Processes , Safety & Mission Assurance , Standard ,

    • NACA-RM-L9E02 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1949
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: INTRODUCTION
      In an attempt to improve the low-speed longitudinal characteristics of sweptback wings, various combinations of high-lift and stall-control devices have been tested in the Langley 19-foot pressure tunnel ...