NASA - National Aeronautics and Space Administration (NASA): Recent submissions
Now showing items 961-980 of 3613
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NASA-LLIS-0377
Abstract: Abstract:
A 21{}hortfall in Voyager's velocity change was suspected to be due to exhaust plume impingement. Due to the complexity of spacecraft/thruster configurations, additional care must be taken ...Subject(s) : Flight Equipment , Spacecraft , -
NASA-LLIS-0220
Abstract: Description of Driving Event:
The logistics and support program for space shuttle is continuing to develop. The problems that persist, in general, are well documented and understood. They do, however, ...Subject(s) : Ground Operations , Logistics , -
NACA-TN-1071
Abstract: INTRODUCTION
A recent investigation (reference 1) was conducted on the NACA 653-018 airfoil section with boundary-layer control by suction to determine the increment in maximum lift coefficient that could ... -
NASA-TN-D-6866
Abstract: A compilation of design considerations applicable to spin-recovery parachute systems for military airplanes has been made so that the information will be readily available to persons responsible for the design of such ...Subject(s) : AERODYNAMIC , AIRCRAFT , CHUTES , CONFIGURATIONS , DEVELOPMENT , DRAG , ENGINEERING , EQUIPMENT , MILITARY , PRODUCT , SPECIFICATIONS , SYSTEMS , -
NASA-LLIS-1169
Abstract: Description of Driving Event:
Not all Aviation Safety Officers (ASOs) Report Directly to Their Center Directors.Subject(s) : Administration/Organization , Aerospace Safety Advisory Panel , Aircraft , Flight Operations , Ground Operations , Policy & Planning , Safety & Mission Assurance , -
NACA-RM-L50K06
Abstract: INTRODUCTION
Previous experimental investigations of the effects of horizontal-tail position on the low-speed static longitudinal stability characteristics of sweptback-wing models (references 1, 2, and 3) have shown ... -
NASA-TN-D-6142
Abstract: Vortex-lattice FORTRAN program for estimating subsonic aerodynamic characteristics of complex planforms.Subject(s) : AERODYNAMIC CHARACTERISTICS , AERODYNAMIC COEFFICIENTS , COMPUTER PROGRAMS , DRAG , FORTRAN , LEADING EDGES , LIFT , PITCHING MOMENTS , PLANFORMS , SUBSONIC SPEED , VORTICES , -
NASA-LLIS-0083
Abstract: Description of Driving Event:
The portable purge unit when operating, exceeds the recommended 85 DBA. Reference is made to noise hazard survey accomplished by BOC industrial hygiene. The noise level ...Subject(s) : Hardware , Industrial Operations , Personal Protective Equipment , -
NASA-LLIS-1017
Abstract: Description of Driving Event:
Application of Systems Engineering Methodology to ISS Caution and Warning System.Subject(s) : Aerospace Safety Advisory Panel , Configuration Management , Human Factors , Risk Management/Assessment , Safety & Mission Assurance , Software , Spacecraft , Standard , Test & Verification , -
NACA-TN-1310
Abstract: Charts providing coefficients for the stress analysis of a reinforced circular cylinder are presented. These charts facilitate the rapid determination of the shear flows and direct stresses in the sheet of the cylinder as ... -
NASA-LLIS-0642
Abstract: Abstract:
Although stainless steel material is generally assumed to be non-magnetic, it is possible for a stainless steel propellant tank to become residually magnetized, either from "working" the ...Subject(s) : attitude control , demagnetization , Helmholtz coil , magnetic compatibility , mission operations , Parts Materials & Processes , Spacecraft , Test & Verification , -
NASA-LLIS-1407
Abstract: Abstract:
Performance of data mining and trending analyses of recurring anomalies in NASA programs are difficult due to numerous and dissimilar Problem Reporting and Corrective Action (PRACA) Databases. ...Subject(s) : Policy & Planning , Program and Project Management , Risk Management/Assessment , Safety & Mission Assurance , -
NACA-RM-A55G19
Abstract: INTRODUCTION
The total resistance of an airfoil may be considered as being composed of two separate components, the drag at zero lift and the drag associated with the production of lift. In the cruising condition the ... -
NASA-LLIS-0396
Abstract: Abstract:
Shortly after transmitter turn-on, SIR-B suffered a radiated power drop. After Shuttle landing, troubleshooting discovered a sliver of metal embedded in the center conductor of the GFE antenna ...Subject(s) : Safety & Mission Assurance , Test & Verification , -
NASA-TN-D-4891
Abstract: Predicting lift and drag for slender sharp-edge Delta wings in ground proximitySubject(s) : AERODYNAMIC , AERODYNAMICS , ANGLE , ATTACK , COEFFICIENTS , DELTA , DRAG , EDGES , EFFECT , FLOW , GROUND , LEADING , LIFT , POTENTIAL , PREDICTIONS , SHARP , VORTICES , WINGS , -
NACA-TN-719
Abstract: An investigation was made in the N.A.C.A. 7- by 10-foot wind tunnel to determine the aerodynamic characteristics of tapered and rectangular wings with partial-span slotted flaps. Two N.A.C.A. 23012 airfoils equipped with ... -
NASA-LLIS-1136
Abstract: Description of Driving Event:
Support for Implementation of Process Control Focus Group for Shuttle Program.Subject(s) : Administration/Organization , Aerospace Safety Advisory Panel , Parts Materials & Processes , Safety & Mission Assurance , -
NASA-LLIS-0844
Abstract: Practice:
Use color coding and identification on piping systems to identify the content and pressure of the contents. -
NACA-TR-934
Abstract: Procedures are recommended for solving the equations of equilibrium of reinforced panels and isolated fuselage rings as represented by the external loads and the operations table established according to Southwell's method. ...Subject(s) : DISPLACEMENT , FUSELAGES , LOAD DISTRIBUTION (FORCES) , MATRICES (MATHEMATICS) , NUMERICAL ANALYSIS , REINFORCED PLATES , REINFORCEMENT RINGS , RELAXATION METHOD (MATHEMATICS) , STRESS ANALYSIS , STRESS CONCENTRATION , STRESSED-SKIN STRUCTURES , -
NASA-LLIS-0057
Abstract: Description of Driving Event:
During the replacement of a faulty flodyne valve, a leak occurred which resulted in a spill of approximately 20 gallons of MMH. Several minutes after the spill was reported, ...Subject(s) : Emergency Preparedness , Energetic Materials - Explosive/Propellant/Pyrotechnic , Fire Protection , Flight Equipment , Ground Equipment , Ground Operations , Hardware , Hazardous/Toxic Waste/Materials , Packaging Handling Storage , Personal Protective Equipment ,

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