... NO . COMBAT MANEUVER SPECIFIC EXCESS POWER 4.0 700 · M = 0.9 • M = 0.9 38 680 • 30,000 FT · 10,000 FT RESERN 3.6 AXI RESERN 660 AXI 3.4 640 32 620 3.0 600 BASE . ALBEN HIGH AR LINE BASE . ALBEN LINE HIGH AR 2.6 COMBAT MANEUVER ...
Thirty-sixth AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and AIAA/ASME Adaptive Structures Forum
... range of half - space velocities , as well as for both transient and steady - state conditions . The so- lutions are presented as both temperature profiles along the heat source centre - line , and as temperature contours on the surface ...
... CAP BULKHEAD RCC NOSE CAP HRSI CIRCUMFERENTIAL DETAIL A THERMAL BARRIER ... wing box front spar using metallic joints to reduce loading on the panels ... ( NC ) and wing leading edge ( WLE ) systems . The LESS qualification systems test ...
... WING PANEL 3 Fig . 3 Space Shuttle Nose Cap and Wing Leading Edge Structural Subsystems The NC and WLE subsystem T / As were designed to include all structural , mechanical , and thermal boundaries essential for a realistic simulation ...
28th AIAA Fluid Dynamics Conference, 4th AIAA Shear Flow Control Conference: June 29-July 2, 1997, Snowmass Village, CO.
... bearing stiffness with speed , however , the rotor weight alone is not sufficient to achieve this eccentricity ... Nomenclature and Parameterization The geometry and relevant nomenclature for a typ- ical journal bearing ( rotating ...
... Near Field Plume. A single PPT Failure Detection and Correction ( FDC ) test is used in the attitude control software ... communication ground pass in Mission Idle Mode Operate in PPT control in Mission Idle Mode for one orbit or greater ...
American Institute of Aeronautics and Astronautics. Editorial The Other Side ... Midnight . " Perhaps the Age of Aquarius has made us all more receptive to see all sides of everything . Anyone can read ... free ! The structure of a technical ...
... models . No entrainment was predicted in this region from the SA model though the velocities are very small and experimental error may be significant . 3. Fountain centerline vertical velocities were best predicted from the CH turbulence ...
... PPT pulse causes the bias voltages to vary . 12 was found to vary by up to ... wiring this experiment to help eliminate as many entry points of noise into ... Power for the PPT and probe motion system were carried on separate feed ...
Proceedings of the ... Annual AIAA/USU Conference on Small Satellites
... Housekeeping Board and the Uplink / Downlink Board . The Spacecraft Processor and Memory Cards provide dual 8085 processors to individually provide telemetry and spacecraft operating system support . Commands are received from the ...
AIAA/ASME/SAE/ASEE 24th Joint Propulsion Conference: July 11-13, 1988, Boston, Massachusetts
... FMI indicator , and sets the appropriate FMI code in the ADAC non - volatile memory . The avionics WRAS functional groups monitored are the following : .. Multi - Function Displays .. .. Data Storage Set Stability ... FMI codes 10.
... ( ASME Y14.5M - 1994 ) ASME Y14.5M - 1994 ... Geometric Symbols , Definitions , and Modifiers ... Material Condition Symbols and Definitions Standard Rules ..... Location Tolerance ... Straightness of a Surface .. Straightness of an Axis ...
AIAA Flight Simulation Technologies Conference: A Collection of Technical Papers
... F- 16D , and the climb performance was recorded . The F- 16C WST was able to ... 16 test . The F - 16C WST had to gradually decrease the flight path angle to ... manual data . It was also difficult to determine if the ModSAF aircraft was ...
The 34th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Adaptive Structures Forum: 93-1370 - 93-1445
... acrylic , in contrast to polycarbonate , showed strong dependence of modulus with strain rate as well as strain . No ... Poisson ratio was essentially constant for polycarbonate and higher than typical 12 handbook values ( 0.39 versus 0.36 ...
40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit July 11-14, 2004, Fort Lauderdale, FL.: 04-4050 - 04-4099
... results agree in every way with actual motor data . C. Results The methods described ... ap- plication of Eq . ( 32 ) in the difficult dilemma repre- sented by ... test series . The progressive pressure rise results from the increasing ...
... ( PPT ) Experiment on the Earth Observing 1 ( EO - 1 ) spacecraft has demonstrated the capability of a new generation PPT to perform spacecraft attitude control . The PPT is a small , self- contained pulsed electromagnetic propulsion ...
... Flow Theory This book is a reprinting of Lagerstrom's Laminar Flow Theory ... incompressible flows , were considered as asymptotic expansions of the exact ... Panton University of Texas STANFORD SIT General Requirements : Send all ...
AIAA Fourth International Aerospace Planes Conference: 92-5036 - 92-5072
... PYRO data shows that TNT equivalence decreases as the weight of the propellant ignited increases . Many of the large scale tests performed during Project PYRO ignited prematurely and the results were not considered in the final analysis ...
JSASS/AIAA/DGLR 17th International Electric Propulsion Conference: Tokyo, 1984
... PPU was enclosed in a compact package ( shown in Fig . 7 ) . The simplified PPU occupies less than one - half of the volume of the IAPS PPU . The new simplified designs have reduced the parts count ... units . Fig . 6 . The IAPS flight unit ...
... OPENLOOP PREDICTED FOR OPENLOOP MEASURED OPENLOOP K TAU 0.80 170.00 TEST # 1 0.77 200.00 TEST # 2 TEST # 2 PREDICTED FOR OPENLOOP TEST # 3 MEASURED OPENLOOP TEST # 3 0.83 170.00 0.78 210.00 0.83 0.83 190.00 230.00 TAUD Kc , max * 3.50 ...
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