NASA Technical Memorandum, Issues 3463-3473; Issues 3475-3480National Aeronautics and Space Administration,., 1976 - Aeronautics |
Other editions - View all
Common terms and phrases
ABS BETAM REL ABS MACH AERONAUTICS AND SPACE airflow ampere-hours angle of attack BETAM REL BETAM blade cells cermets COEFF TOT PROF coefficient combustor compressor configuration D-FACT EFF RP delta wing design speed DEV D-FACT EFF dihedral angle efficiency electrodes elevon surfaces emission end plate attached end-plate surface engine speed equation fuel FWGV heat pipe INCIDENCE DEV D-FACT ion thrusters kilograms Lewis Research Center LOSS COEFF TOT LOSS PARAM TOT Mach number mass megapascal MERID MACH MERID PEAK SS NASA NASA TM NATIONAL AERONAUTICS oxidation PARAM TOT PROF PERCENT INCIDENCE DEV Percent of design pressure ratio propulsion module radiation recirculation reference REL MACH rotor schlieren shown in figure skewed slot solar array spacecraft SPAN MEAN SS speckle stator submodules TABLE thermal thruster tip clearance TOTAL PRESS TOTAL TEMP TSSM tube turbine V-tail WHEEL SPEED wing and elevon WT FLOW
Popular passages
Page 47 - 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.
Page 10 - AMES RESEARCH STAFF : Equations, Tables, and Charts for Compressible Flow. NACA Rep. 1135, 1953.
Page 10 - Characteristics of Major Active Wind Tunnels at the Langley Research Center,