NASA - National Aeronautics and Space Administration (NASA): Recent submissions
Now showing items 2881-2900 of 3613
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NASA-TP-1498
Abstract: An investigation was conducted in the Langley low-turbulence pressure tunnel to determine the low-speed two-dimensional aerodynamic characteristics of a 13-percent-thick medium-speed airfoil designed for general aviation ...Subject(s) : AERODYNAMIC , AIRCRAFT , ANGLE , ATTACK , AVIATION , CHARACTERISTICS , DESIGN , GENERAL , MACH , NUMBER , REYNOLDS , TESTS , TUNNEL , WIND , -
NASA-LLIS-1293
Abstract: Description of Driving Event:
In order to mitigate the risk associated with flying a high-performance technology demonstrator, the Project chose to build two aircraft (a primary and a backup) and operate ...Subject(s) : Aerospace Safety Advisory Panel , -
NACA-RM-L54F25
Abstract: INTRODUCTION
Various investigations have been conducted that are concerned with the aerodynamic characteristics of the Douglas D-558-II research airplane which is currently undergoing flight tests by the NACA High-Speed ... -
NASA NPD 3410.2 REV F
Abstract: APPLICABILITY
This NPD applies to NASA Headquarters and NASA Centers, including Component Facilities, except the Office of the Inspector General which may implement the policy through its own personnel ... -
NACA-TR-1181
Abstract: An analysis is made of the structural response to gusts of an airplane having the degrees of freedom of vertical motion and wing bending flexibility and basic parameters are established. A convenient and accurate numerical ...Subject(s) : AIRCRAFT , AIRCRAFT STRUCTURES , COMPARISON , DISPLACEMENT , DYNAMIC RESPONSE , DYNAMIC STRUCTURAL ANALYSIS , FLEXIBILITY , FLIGHT TESTS , GUST LOADS , GUSTS , NUMERICAL ANALYSIS , THEORIES , WINGS , -
NASA NPD 4100.1 REV B
Abstract: Applicability
This policy is applicable to NASA Headquarters and NASA Centers, including Component Facilities. These provisions are to be made applicable, through its contract, to any on-site contractor: ... -
NASA-TN-D-3580
Abstract: Discrepancies between wind tunnel predictions and actual flight test results for conditions of supercritical separated flow. -
NASA-LLIS-0331
Abstract: Description of Driving Event:
The Hubble Space Telescope did not perform to the requirements of the contract. A spherical aberration was attributed to the spacing between the field lens and the lower ...Subject(s) : Safety & Mission Assurance , -
NASA-LLIS-2136
Abstract: Abstract:
The early work of the Exploration Systems Mission Directorate (ESMD) focused on human factors engineering (i.e., applying what is known about human capabilities and limitations to the design ...Subject(s) : Engineering Design (Phase C/D). , Engineering Design (Phase C/D).Launch Systems , Integration and Testing , Manufacturing and Assembly , Mission Operations and Ground Support Systems. , Mission Operations and Ground Support Systems.Ground support systems , Missions and Systems Requirements Definition. , Missions and Systems Requirements Definition.Human factors impact on mission design , Safety and Mission Assurance. , Safety and Mission Assurance.Impact of human factors on systems requirements and designs , Systems Engineering and Analysis. , Systems Engineering and Analysis.Human factors planning , -
NASA-LLIS-1063
Abstract: Description of Driving Event:
Lack of Systems Engineering in ISS Caution and Warning (C&W) System Design.Subject(s) : Aerospace Safety Advisory Panel , Human Factors , Information Technology/Systems , Policy & Planning , Research & Development , Risk Management/Assessment , Safety & Mission Assurance , Software , Spacecraft , Test & Verification , -
NASA-LLIS-6376
Abstract: The attached report will make a cursory look at the various elements of how programs and projects understand and manage engineering the system and technical integration. Approximately 80% of the problems encountered in ... -
NACA-RM-A7K28
Abstract: INTRODUCTION
This report present the high-speed stability and control characteristics of a fighter airplane model with a 35° swept-back wing and tail. The data presented herein were obtained form ... -
NASA-LLIS-0678
Abstract: Practice:
This guideline provides information and guidance for the design of thick-film hybrid circuits. -
NASA-LLIS-1522
Abstract: Abstract:
The Orbital Space Plane (OSP) Program technical content and review standards were diluted as the program accelerated and budgets adjusted. Development of a minimum set of NASA-preferred design ...Subject(s) : Administration/Organization , Communication Systems , NASA Standards , -
NASA-LLIS-1725
Abstract: Abstract:
Significant leakage or "blow-by" of combustion products past the seals within a pyrotechnic cable cutter was detected during pyroshock testing of Mars Exploration Rover. Optical flight ...Subject(s) : Additional Categories. , Additional Categories.Energetic Materials Explosive/Propelland/Pyrotechnic , Additional Categories.Flight Equipment , Additional Categories.Hardware , Additional Categories.Parts , Materials & Processes , Additional Categories.Payloads , Additional Categories.Risk Management/Assessment , Additional Categories.Spacecraft , Additional Categories.Test & Verification , Additional Categories.Test Article , Engineering Design (Phase C/D). , Engineering Design.Power , Program Management. , Program Management.Risk management , Safety and Mission Assurance. , Safety and Mission Assurance.Advance planning of safety systems , Safety and Mission Assurance.Product Assurance , -
NASA NPR 9620.1
Abstract: PURPOSE
This NASA Procedural Requirements (NPR) document provides general principles, standards, policies, and procedures to assure compliance with statutory and regulatory requirements for the pay, ... -
NACA-RM-A51H20 REV A
Abstract: INTRODUCTION
The scoop-type inlet and the NACA submerged inlet are two current inlet designs which supply air to a jet engine and require a relatively short internal ducting. An NACA submerged inlet has been previously ... -
NASA-LLIS-0443
Abstract: Description of Driving Event:
During the removal of power to a transformer prior to it being serviced, an accidental 2400 Volt line to ground short circuit was created resulting in minor injury to a ...Subject(s) : Configuration Management , Energy , Logistics , Safety & Mission Assurance , -
NASA-LLIS-0244
Abstract: Description of Driving Event: Prior to being operated at KSC, SKYLAB hydraulic systems were tested for contamination. If the systems were found to be clean, they were sealed and not retested. After being ...Subject(s) : Flight Equipment , Hardware , Launch Vehicle , Parts Materials & Processes , Spacecraft , -
NASA-LLIS-1260
Abstract: Description of Driving Event:
On 24 April 2002, 7:35 a.m. (CST) two employees, working in a Clean Room configured for glass inspection and assembly, were rotating a Flight Cupola Trapezoidal Debris ...Subject(s) : Configuration Management , Flight Equipment , Flight Operations , Ground Equipment , Ground Operations , Hardware , Industrial Operations , Parts Materials & Processes , Risk Management/Assessment , Test & Verification ,

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