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

Now showing items 1161-1180 of 3613

    • NASA-LLIS-1273 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2002
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      The UTMC UT69R000 (aka ut69r, r000) microprocessor has several known problems that users must be aware of.
      Subject(s) : Flight Equipment ,

    • NACA-TN-3615 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1956
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: An experimental investigation was made to determine the scale effects of the forces from water spray generated by a flat rectangular planing surface and impinging on a collector plate representative of an aerodynamic surface ...

    • NASA-CR-3808 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1984
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: This paper describes methodology and an associated computer program for the design of wing lifting surfaces with attainable thrust taken into consideration. The approach is based on the determination of an optimum combination ...
      Subject(s) : AERODYNAMIC , ANALYSIS , CAMBERED , COEFFICIENTS , COMPUTER , DESIGN , DRAG , EDGE , FLOW , LEADING , LINEARIZATION , NUMERICAL , PROFILES , PROGRAMS , REDUCTION , SUBSONIC , SUPERSONIC , THRUST , WING , WINGS ,

    • NASA NPR 2570.1 REV B 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2008
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: PURPOSE
      This NPR sets forth the procedures for the management requirements for establishing and governing the use of radio frequencies by the National Aeronautics and Space Administration (NASA).
      NPR ...

    • NASA-LLIS-0128 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1992
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      MLG tire heat generated from max. Braking due to a crosswind landing, heavy orbiter, or long landing, could cause a transfer of heat to continue to the MLG tires after ...
      Subject(s) : Fire Protection , Flight Equipment , Ground Operations ,

    • NASA-STD-8719.13 REV C 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2013
      Organization : NASA - National Aeronautics and Space Administration (NASA)

    • NASA-LLIS-1129 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1999
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      Need to Upgrade International Space Station (ISS) Command and Data Handling (C&DH) Components as Soon as Possible
      Subject(s) : Aerospace Safety Advisory Panel , Computers , Information Technology/Systems , Software , Spacecraft ,

    • NASA NPD 8730.5 REV B W/CHG 2 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2011
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: APPLICABILITY
      a. This NPD applies to NASA Headquarters and Centers, including Component Facilities, and to the Jet Propulsion Laboratory and other NASA contractors and grantees as specified in their ...

    • NACA-TM-1122 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1947
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Wind-tunnel measurements on projectiles are discussed. Tests at the Gottingen Tunnel are described. The tunnel operates on the Prandtl principle, that is, a brief stationary air stream produced in an evacuated tank by ...
      Subject(s) : AIR , ANGLE , ATTACK , FLOW , MATHEMATICAL , MISSILES , MODELS , PROJECTILES , TESTS , TUNNEL , WIND ,

    • NASA-LLIS-0692 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2000
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Practice:
      This guideline provides a procedure which specifies and documents consistent, useful, and welldefined coordinate system (or frame) definitions for spacecraft attitude control design and ...

    • NACA-TR-665 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1939
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Factors derived from wing theory are presented. By means of these factors, the angle of zero lift, the lift-curve slope, the pitching moment, the aerodynamic-center position, and the induced drag of tapered wings with ...

    • NASA-LLIS-1579 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2005
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Abstract:
      Building was not properly decommissioned. GSFC did not have formal procedures for decommissioning and transfer of ownership of buildings and/or systems (includes utilities, pneumatics and ...
      Subject(s) : Facilities ,

    • NASA-LLIS-0931 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2000
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      JSC employees fell out of their office chairs when they broke. One employee was injured; the other was not. These two events were several months apart.
      The model that ...
      Subject(s) : Environment , Facilities , Hardware , Human Factors , Logistics , Occupational Health , Procurement Small Business & Industrial Relations ,

    • NASA-TM-X-3437 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1977
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: An experimental investigation was conducted in the Ames 12-Foot Wind Tunnel to determine the subsonic aerodynamic characteristics, at high angles of attack, of a tangent ogive forebody with a fineness ratio of 3.5. The ...
      Subject(s) : AERODYNAMIC , ANGLE , ATTACK , BODIES , CHARACTERISTICS , FORCES , FOREBODIES , MACH , NUMBER , OGIVES , REVOLUTION , REYNOLDS , SIDESLIP , TESTS , TUNNEL , WIND , YAW ,

    • NACA-TN-3481 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1955
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: An investigation was made at a Mach number of 0.13 in the Langley stability tunnel in order to determine the effects of closed wing-root air ducts (horizontal) on the static longitudinal and static lateral stability ...

    • NASA-RP-1046 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1980
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Problems involved in measuring speed and altitude with pressure-actuated instruments (altimeter, airspeed indicator, true-airspeed indicator, Machmeter, and vertical-speed indicator) are examined. Equations relating total ...
      Subject(s) : ACCURACY , AIRCRAFT INSTRUMENTS , AIRSPEED , CALIBRATING , FLIGHT ALTITUDE , PRESSURE MEASUREMENT , STATIC PRESSURE ,

    • NASA-LLIS-0508 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1994
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      Currently, only one method is available for determining an object's angle of impact against a structure: high speed photography. This method requires a great deal of ...
      Subject(s) : Research & Development ,

    • NASA-TN-D-3583 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1966
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Influence of ground induced aerodynamic effects on landing maneuver of aircraft with low aspect ratio wings
      Subject(s) : AERODYNAMICS , AIRCRAFT , ASPECT , EFFECT , GROUND , LANDING , LOW , RATIO , WING , WINGS ,

    • NASA-LLIS-1334 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;2003
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Description of Driving Event:
      The propellant tanks on the Genesis spacecraft were filled with isopropyl alcohol (IPA) prior to modal and acoustic vibration testing in order to obtain the proper spacecraft ...
      Subject(s) : alcohol flush , cleanliness verification , decontamination , environmental test , Flight Equipment , Hardware , Parts Materials & Processes , Pressure Vessels , Spacecraft , Test Article ,

    • NACA-TN-646 

      Type: standard
      Source: NASA - National Aeronautics and Space Administration (NASA):;1938
      Organization : NASA - National Aeronautics and Space Administration (NASA)
      Abstract: Wind tunnel tests of a 15-foot-span model of a two-engine low wing transport airplane were made as a preliminary study of the emergency arising from the failure of one engine in flight. Two methods of reducing the initial ...