NASA - National Aeronautics and Space Administration (NASA): Recent submissions
Now showing items 3341-3360 of 3613
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NASA-LLIS-1504
Abstract: Abstract:
The Orbital Space Plane (OSP) Program technical content and review standards were diluted as the program accelerated and budgets adjusted. Altered plans produce altered results. Address ...Subject(s) : Administration/Organization , Policy & Planning , Program and Project Management , -
NASA-TP-2990
Abstract: Experimental and theoretical aerodynamic characteristics were compared for a high-lift, semispan wing configuration that incorporated a slightly modified version of the NASA Advanced Laminar Flow Control airfoil section. ...Subject(s) : AERODYNAMIC , AIRFOIL , BOUNDARY , CHARACTERISTICS , COMPUTER , CONFIGURATIONS , CONTROL , DISTRIBUTION , DRAG , DYNAMICS , EDGES , FLOW , FLUID , LAMINAR , LAYER , LEADING , LIFT , METHOD , MODELS , MOMENT , NUMBER , PANEL , PRESSURE , PROFILES , PROGRAMS , REYNOLDS , SEMISPAN , SEPARATED , SUBSONIC , TUNNELS , WIND , -
NASA-TN-D-55
Abstract: An investigation has been made in the 17-foot test section of the Langley 300-MPH 7- by 10-foot tunnel to determine the longitudinal aerodynamic characteristics of tilt-wing, deflected-slipstream, and combination tilt-wing ...Subject(s) : AERODYNAMIC , AERODYNAMICS , AIRCRAFT , CHARACTERISTICS , CONFIGURATIONS , EFFECT , GROUND , PROPELLERS , TAKEOFF , TESTS , TUNNEL , VERTICAL , WIND , -
NASA-CR-2270
Abstract: The hydrodynamic theory of the extreme pool boiling heat fluxes is expanded to embrace a variety of problems that have not previously been analyzed. These problems include the prediction of the peak heat flux on a variety ...Subject(s) : ELECTROLYSIS , FILM BOILING , HEAT FLUX , HEAT GENERATION , HEATING EQUIPMENT , MATERIALS TESTS , MICROGRAVITY , THERMODYNAMIC PROPERTIES , -
NASA-LLIS-0490
Abstract: Description of Driving Event:
International travelers should be prepared to deal with grounding problems that have been experienced by NASA personnel. As an example, several personnel have been ...Subject(s) : Energy , Facilities , -
NASA-LLIS-0262
Abstract: Abstract:
The magnitude of both the real-time cruise activities and the work required to perform advanced planning for future activities, such as encounter, landing site certification, test and training, ...Subject(s) : Administration/Organization , Policy & Planning , -
NASA-TP-1435
Abstract: INTRODUCTION
Experimental data for scale-model aircraft are used to define the aerodynamic characteristics of full-scale aircraft, verify theoretically predicted aerodynamic characteristics, and provide data where ... -
NASA-LLIS-1301
Abstract: Description of Driving Event:
The science team was not an active participant in the mission development, due to an ill-defined role and corresponding lack of budget.Subject(s) : Administration/Organization , -
NACA-RM-L54E19 REV A
Abstract: INTRODUCTION
The design of the internal-flow system of a turbojet-powered aircraft for optimum operation at transonic or supersonic speeds tends to compromise the operation of the system at conditions corresponding to ... -
NASA-LLIS-6657
Abstract: Use of a multi-mission operations system has permitted new NASA projects to reduce the cost, schedule, and risk of developing such systems anew, while improving mission performance. Projects should be AMMOS "capability-driven," ... -
NACA-TR-1170
Abstract: A review is presented of available information on the behavior of brittle and ductile materials under conditions of thermal stress and thermal shock. For brittle materials, a simple formula relating physical properties to ...Subject(s) : AGING (MATERIALS) , ANALYSIS (MATHEMATICS) , BRITTLE MATERIALS , DUCTILITY , FRACTURE STRENGTH , METALS , SHOCK RESISTANCE , STRESS ANALYSIS , STRESS CONCENTRATION , THERMAL EXPANSION , THERMAL STRESSES , THERMODYNAMIC PROPERTIES , -
NASA NPR 5900.1
Abstract: Purpose
This NPR provides internal guidance in the following areas for Agencywide roles in procuring spare parts:
Program
Procurement
Logistics
Engineering
Applicability ... -
NASA-TN-D-3149
Abstract: Variable amplitude axial load fatigue test on notched aluminum alloy specimens - aircraft component testing.Subject(s) : AIRCRAFT PART , AIRCRAFT PARTS , ALUMINUM ALLOY , ALUMINUM ALLOYS , AXIAL LOAD , AXIAL LOADS , FATIGUE TEST , FATIGUE TESTS , LOAD TESTS , LOADS (FORCES) , METAL FATIGUE , NOTCH TESTS , NOTCHED METAL , -
NASA-LLIS-0330
Abstract: Description of Driving Event:
KSC post flight inspections of RSRM-2 (STS 27) showed a 3.5" x 3.5" piece of JPS cork missing from the right hand center field joint at 185 degrees indicating debris. An ...Subject(s) : Hardware , Parts Materials & Processes , -
NASA-LLIS-2116
Abstract: Abstract:
Many spacecraft include mission operations that implement an irreversible process(s) (e.g. pyro technical deployments) which changes the state or configuration of the spacecraft and its ...Subject(s) : Engineering Design (Phase C/D).Spacecraft and Spacecraft Instruments , Integration and Testing , Manufacturing and Assembly , -
NASA-LLIS-0989
Abstract: Description of Driving Event:
The ETU Laser for GLAS started showing signs of failing to lase. Initial failure investigations pointed to the laser Oscillator Diode. A detailed investigation disclosed ...Subject(s) : Configuration Management , Flight Equipment , Hardware , Parts Materials & Processes , Risk Management/Assessment , Safety & Mission Assurance , Spacecraft , Test & Verification , -
NACA-RM-A7K24
Abstract: INTRODUCTION
An investigation bf. the theoretical prediction of control surface hinge moments by lifting-surface theory has been undertaken by the NACA. The 1fftIn~UTface theory is a further refinement to the lifting-line ... -
NASA-LLIS-0677
Abstract: Practice:
Thoroughly test high voltage power supply packaging on flight configured engineering models, in a simulated space flight environment, to evaluate corona effects. -
NASA-LLIS-1721
Abstract: Abstract:
A system of pre-start tasks ane emergency plannning ameliorated the effects of an arc blast to an employee.Subject(s) : Additional Categories. , Additional Categories.Emergency Preparedness , Additional Categories.Facilities , Additional Categories.Human Factors , Additional Categories.Human Resources & Education , Additional Categories.Industrial Operations , Additional Categories.Personal Protective Equipment , Additional Categories.Policy & Planning , Additional Categories.Risk Management/Assessment , Additional Categories.Safety & Mission Assurance , -
NASA-LLIS-1521
Abstract: Abstract:
A history of commanding anomalies experienced by the Mars Global Surveyor, Stardust, Mars Odyssey, and Genesis missions prompted JPL to perform a comprehensive review of the command uplink ...Subject(s) : command failures , Communication Systems , erroneous commanding , Flight Operations , flight team anomalies , Ground Operations , Information Technology/Systems , mission operations , operations assurance , operations procedures , operations training , Safety & Mission Assurance , Software , Spacecraft , Test & Verification ,

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