NASA Technical NoteNational Aeronautics and Space Administration., 1972 |
طبعات أخرى - عرض جميع المقتطفات
عبارات ومصطلحات مألوفة
abort AERONAUTICS AND SPACE airplane amplitude analog computer autothrottle B-2 test baffle bypass door C-2 engine calculated Centaur tank chamber pressure composites condition contribution to existing deployment detector digital computer Elementary Processes engine firing equation experimental facility flight frequency fuel pump function heat pipes heaters helium hydrogen tank pressurization input laser lidar limit cycle liquid hydrogen liquid oxygen tank Mach measured meganewtons meters mode-locked molybdenum N/cm N/cm² NASA NASA TN NATIONAL AERONAUTICS operation output Oxidizer parameter percent photodiode photomultiplier pilot parachute pressurant gas pressurization system prestart prevalve propellant tank psia pulse pump inlet reactor Report resonance integral response RL10 engines sample saturation pressure SCIENTIFIC AND TECHNICAL sequence shown in figure signal SPACE ADMINISTRATION WASHINGTON Spacecraft Propulsion spin spin-recovery parachute spray chamber static pressure steady-state storage superalloys temperature test program thermal Type ullage ullage pressure valve vehicle velocity wire workload
مقاطع مشهورة
الصفحة 2 - The units for the physical quantities defined in this paper are given in the International System of Units (SI) and parenthetically in US Customary Units.
الصفحة 1 - SYMBOLS Physical quantities in this report are given in the International System of Units (SI) and parenthetically in US Customary Units. The measurements were taken in US Customary Units.
الصفحة 27 - Laboratory at Marshall Space Flight Center has been actively engaged in such observations using image orthicons and intensified SEC vidicons. The results of these observations are presented along with an interpretation in terms of mass-flux. This interpretation includes the development of a relationship between peak luminosity of a meteor and mass, velocity, and zenith angle that was derived from single body meteor theory and compares favorably with results obtained from the Artificial Meteor Program....
الصفحة 21 - Forces on Cylinders and Plates in an Oscillating Fluid,
الصفحة 13 - Laser oscillations in Nd-doped yttrium aluminum, yttrium gallium and gadolinium garnets Appl.
الصفحة 20 - Dynamic Response of Airplanes to Atmospheric Turbulence Including Flight Data on Input and Response," NASA TR R-199, June 1964 (initially presented as an AGARD paper, July 1962).