Static and dynamic characteristics of Centaur gimbal system under thrust load
Static and dynamic characteristics of Centaur gimbal system under thrust loading
STATIC TESTING↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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An empirical method for determining static distributed aerodynamic loads on axisymmetric multistage launch vehicles
Empirical method for determining static distributed aerodynamic loads on axisymmetric multistage launch vehicles
AERODYNAMIC LOAD↗
Wind-tunnel investigation at high subsonic speeds of the effects on static stability characteristics of various modifications to a swept-wing fighter-type airplane model
Wind tunnel investigations of effect on static stability of modifications to swept wing fighter aircraft model
STATIC STABILITY↗
Improvement of propeller static thrust estimation Final report, Jul. 1, 1964 - Aug. 31, 1965
Research facility development for propeller thrust and torque measurements under static thrust conditions
PROPELLER DRIVE↗
Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a V/STOL airplane configuration with a variable-sweep wing and with a skewed wing design
Static longitudinal and lateral aerodynamic characteristics of V/STOL aircraft with variable sweep wing
AERODYNAMIC CHARACTERISTICS↗
Saturn S-IB stage Final static test report, stage S-IB-4
Acceptance static test firing data for Saturn flight stage S-IB-4
ROCKET FIRING↗
Static aerodynamic characteristics of the aborted Apollo-Saturn IB vehicle
Static aerodynamic characteristics of aborted Apollo-Saturn vehicles with normal force coefficient distributions
SATURN IB LAUNCH VEHICLE↗
Design, development and delivery of one /1/ breadboard and three /3/ production units of A 75 VA integrated static inverter Monthly progress report no. 10, Feb. 1966
Breadboard design and production units of integrated static inverter
STATIC INVERTER↗
Development of reliability methodology for systems engineering. Volume II - Application - Design reliability analysis of a 250 volt-ampere static inverter Final report
Design stage reliability analysis application to static inverter
RELIABILITY↗
The predictability of wind and virtual temperature profiles for flight and static test operations Final report, Jul. 1, 1965 - Mar. 31, 1966
Predictability of wind and virtual temperature profiles for flight and static test operations
TEMPERATURE PROFILE↗
Design, development and delivery of one /1/ breadboard and three /3/ production units of a 75 VA integrated static inverter Monthly progress report no. 11, Mar. 1966
Breadboard model development of integrated static inverter
STATIC INVERTER↗
Aerodynamic Performance and Static Stability and Control of Flat-Top Hypersonic Gliders at Mach Numbers from 0.6 to 18
Aerodynamic performance characteristics and static stability and control of hypersonic glider with arrow planform wings
HYPERSONIC GLIDER↗
Static stability and control characteristics of two large-dihedral right triangular pyramid lifting reentry configurations at a Mach number of 3.05
Static stability and control characteristics of dihedral right triangular pyramid lifting reentry vehicle configurations
REENTRY VEHICLE↗
Transonic static and dynamic longitudinal stability characteristics of a low-fineness- ratio, blunted-cylinder reentry body having a converging-cone afterbody
Transonic static and longitudinal stability characteristics of low fineness ratio, blunted cylinder reentry body with converging cone afterbody
BLUNT BODY↗
Static longitudinal, directional, and lateral stability and control data at a Mach number of 6.83 of the final configuration of the X- 15 research airplane
X-15 aircraft static longitudinal, directional, and lateral stability and control at hypersonic speeds
HYPERSONIC SPEED↗
Low-speed investigation of effects of vertical tails on the static stability characteristics of a canard-bomber configuration having a very thin wing and a slender elliptical fuselage
Effect of vertical tails on low speed static stability characteristics of canard-bomber configuration with very thin wing and slender elliptical fuselage
BOMBER AIRCRAFT↗
Static stability characteristics of cone and half-cone-pyramid configurations at Mach 6.83
Longitudinal and static stability characteristics of cone and half-cone with rectangular pyramid configurations
STATIC STABILITY↗
Transonic Wind-tunnel Investigation of Static Longitudinal and Lateral Stability and Control Characteristics and Drag Rise of a Representative Fighter Airplane
Transonic wind tunnel study of static longitudinal and lateral stability and control characteristics and drag rise of fighter aircraft
STATIC STABILITY AND CONTROL↗