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

Now showing items 1121-1140 of 3613

    • NASA-LLIS-0862 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2000
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      Test personnel from the 3.5-foot Hypersonic Wind Tunnel facility, supported by personnel from the project phase 3 contractor, were conducting blowdown tests as a part of ...
      Subject(s) : Aircraft , Ground Equipment , Test Facility ,

    • NASA-LLIS-5479 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2011
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Metal bellows flex hoses are very susceptible to reverse bending low cycle fatigue which results in leakage via a through crack in the bellows.
      Subject(s) : 0.Environmental Control and Life Support Systems , 1.Aircraft , 1.Computer-Aided Design/Manufacturing/Engineering , 1.Cryogenic Systems , 1.Early requirements and standards definition , 1.Facilities , 1.Ground Equipment , 1.Ground Operations , 1.Ground processing and manifesting , 1.Ground support systems , 1.Hardware , 1.Human factors planning , 1.Industrial Operations , 1.Launch support systems , 1.Launch Vehicle , 1.Logistics , 1.Logistics and maintenance , 1.Lunar Operations , 1.Maintenance , 1.Packaging , Handling , Storage , 1.Parts , Materials , & Processes , 1.Planetary entry and landing concepts , 1.Pressure Vessels , 1.Quality , 1.Reliability , 1.Risk Management/Assessment , 1.Safety & Mission Assurance , 1.Spacecraft , 1.Test & Verification ,

    • NASA-LLIS-0388 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1995
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Abstract:
      When large strips of conformal coating were removed from Galileo CDS boards, the process caused the coating to expand and stress the solder joints. The recommendations provide cautions on ...
      Subject(s) : Parts Materials & Processes , Repair ,

    • NASA-LLIS-0192 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1992
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      Photoanalysis of the STS-28 (OV-102, Columbia) flight showed larger body flap deflections than were calculated. The flaps are in a turbulent flow field, which creates a ...
      Subject(s) : Flight Equipment , Launch Vehicle , Test & Verification ,

    • NACA-TN-659 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1938
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: A large-chord NACA 23012 airfoil was tested. The airfoil extended completely across the test section, and two-dimensional flow was approximated. The model was fitted with a full-span slotted flap having a chord 25.66 percent ...

    • NASA-LLIS-1212 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1998
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      During functional test of the Qualification Model of the Mobile Transporter (MT) Linear Drive Unit (LDU), mounted on the Functional Test Fixture (FTF) a power surge followed ...
      Subject(s) : Computer-Aided Design/Manufacturing/Engineering , Configuration Management , Flight Equipment , Flight Operations , Ground Equipment , Ground Operations , Hardware , Independent Verification and Validation , Parts Materials & Processes , Policy & Planning , Risk Management/Assessment , Safety & Mission Assurance , Test & Verification , Test Article , Test Facility ,

    • NASA-LLIS-0847 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2000
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Practice:
      Use ultrasound as a technique for detection of air/fluid leaks, electrical shorts and bearing wear in Ground Support Equipment (GSE). Ultrasound is a technique of listening for audible ...

    • NACA-TR-479 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1935
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: In this report a theoretical solution is developed for the torsion on a round thin-walled tube for which the walls become unstable. The results of this theory are given by a few simple formulas and curves which cover all ...
      Subject(s) : BUCKLING , CIRCULAR TUBES , COMPARISON , CRITICAL LOADING , CURVES , DEFLECTION , DIFFERENTIAL EQUATIONS , EQUILIBRIUM EQUATIONS , EXPERIMENTATION , FAILURE , FORMULAS , PIPES (TUBES) , TEST EQUIPMENT , THEORIES , THIN WALLS , TORSIONAL ,

    • NASA-LLIS-0048 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1991
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      The Firex system components at the VPF are missing numerous identification/find number tags. These are used to identify components in procedures and work authorization ...
      Subject(s) : Configuration Management , Facilities , Fire Protection , Ground Equipment , Ground Operations , Hardware , Industrial Operations ,

    • NASA-LLIS-0985 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2001
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      During Space Station hardware testing at Kennedy Space Center, a technician was in the process of connecting a current probe banana type plug test lead into a breakout box ...
      Subject(s) : Facilities , Ground Equipment , Ground Operations , Industrial Operations , Logistics , Payloads , Research & Development , Safety & Mission Assurance , Test & Verification , Test Article , Test Facility ,

    • NASA-STD-2804 REV FY2014 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2013
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Purpose
      This Standard defines the baseline software suite necessary to support interoperability both between NASA end user computers and within the NASA operating environment. The Standard establishes ...

    • NASA-LLIS-0594 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1998
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      The SEPICA instrument, one of 9 instruments flown on the ACE Mission, uses isobutane gas as part of its particle detection scheme. Three proportional counters, one associated ...
      Subject(s) : Hardware , Procurement Small Business & Industrial Relations , Risk Management/Assessment , Test & Verification ,

    • NASA-LLIS-1437 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2003
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Abstract:
      NASA needs to understand that a human space flight accident field recovery operation will involve many organizations at various levels of Government.
      Subject(s) : Accident Investigation , Administration/Organization , NASA Standards , Policy & Planning , Safety & Mission Assurance ,

    • NASA-LLIS-0875 

      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 May 16, 1994, an AMDAHL 5995M mainframe computer overheated at approximately 8:20 AM in the Software Production Facility (SPF) in Building 30 at JSC. Physical damage ...
      Subject(s) : Administration/Organization , Communication Systems , Computers , Configuration Management , Emergency Preparedness , Energy , Environment , Facilities , Ground Equipment , Ground Operations , Hardware , Industrial Operations , Information Technology/Systems , Occupational Health , Policy & Planning , Risk Management/Assessment , Safety & Mission Assurance , Security , Test & Verification , Test Article , Test Facility , Training Equipment ,

    • NACA-TN-1977 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1949
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: INTRODUCTION
      The linearized theory for supersonic flow has been used by various investigators to develop expressions for the stability derivatives. The information is scattered, however, through a number of reports, ...
      Subject(s) : CHARACTERISTICS , DAMPING , DELTA , EDGES , LATERAL , LEADING , RECTANGULAR , ROLL , STABILITY , SWEPTBACK , TAPERED , WINGS ,

    • NASA-TM-X-2163 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1971
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Transonic and supersonic dynamic stability characteristics of variable sweep wing tactical fighter aircraft
      Subject(s) : AIRCRAFT , ANGLE , ATTACK , DYNAMIC , FIGHTER , FLOW , MACH , MODELS , NUMBER , STABILITY , SUPERSONIC , SWEEP , TESTS , TRANSONIC , TUNNEL , VARIABLE , WIND , WINGS ,

    • NASA-LLIS-0168 

      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 three inch diameter stainless steel manifold containing hydrogen (0.27 lbs) and air (0.26 lbs) at 350 psia ruptured during experimental operation. The hardware was ...
      Subject(s) : Energetic Materials - Explosive/Propellant/Pyrotechnic , Test & Verification ,

    • NACA-TM-948 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1940
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: The approximation method described makes possible lift-distribution computations in a few minutes. Comparison with an exact method shows satisfactory agreement. The method is of greater applicability than the exact method ...

    • NASA-LLIS-1011 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1997
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      Transition to USA Management of Logistics Functions Under Phase 1 of the SFOC Contract.
      Subject(s) : Administration/Organization , Aerospace Safety Advisory Panel , Ground Operations , Logistics ,

    • NASA-LLIS-0810 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2000
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Practice:
      As a minimum, run eight thermal cycles over the approximate temperature range for hardware that cycles in flight over ranges greater than 20oC. The last three thermal cycles should ...