000 -LEADER |
fixed length control field |
02489nam a22002777a 4500 |
003 - CONTROL NUMBER IDENTIFIER |
control field |
OSt |
040 ## - CATALOGING SOURCE |
Transcribing agency |
IIT Kanpur |
041 ## - LANGUAGE CODE |
Language code of text/sound track or separate title |
eng |
245 ## - TITLE STATEMENT |
Title |
NASA Technical Note [D-2701-2710] |
260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) |
Place of publication |
Washington |
Name of publisher |
National Aeronautics and Space Administration (NASA) |
Year of publication |
1965 |
490 ## - SERIES STATEMENT |
Series statement |
National Aeronautics and Space Administration (NASA) |
-- |
NASA Technical Note |
500 ## - GENERAL NOTE |
General note |
NASA TN D-2701: Effects of Lateral control, characteristics on hovering: jet lift vtol aircraft/ by L. Stewart Rolls, Fred J. Drinkwater III and Robert C. Innis |
500 ## - GENERAL NOTE |
General note |
NASA TN D-2702: Impact of V / STOL aircraft on instrument weather operations/ John P. Reeder |
500 ## - GENERAL NOTE |
General note |
NASA TN D-2703: Description and initial calibration of the langley 12-inch Hypersonic ceramic-heated tunnel/ Louis E. Clark |
500 ## - GENERAL NOTE |
General note |
NASA TN D-2704: Hemispherical spectral emittance of ablation chars, carbon, and zirconia to 3700 degree K / by R. Gale Wilson |
500 ## - GENERAL NOTE |
General note |
NASA TN D-2705: results of USAF-NASA-FAA flight program to study community responses to sonic booms in the greater St. Louis Area/ by Charles W. Nixon, Harvey H. Hubbard |
500 ## - GENERAL NOTE |
General note |
NASA TN D-2706: Effect of surface emittance on turbulent skin friction at supersonic and low hypersonic speeds/ Jerry M. Allen and K. R. Czarnecki |
500 ## - GENERAL NOTE |
General note |
NASA TN D-2707: Fixed- base simulator study of piloted entry into the earth's atmosphere at parabolic velocity/ by Martin T. Moul and Albert A. Schy |
500 ## - GENERAL NOTE |
General note |
NASA TN D-2708: Study of pressure and heat transfer over an 80 degree sweep slab delta wing in hypersonic flow/ Allen H. Whitehead and James C. Dunavant |
500 ## - GENERAL NOTE |
General note |
NASA TN D-2709: Effect of first-stage geometry on aerdynamic characteristics in pitch of two-stage rocket vehicles from mach 1.57 to 2.86/ by William A. Corlett and Celia S. Richardson |
500 ## - GENERAL NOTE |
General note |
NASA TN D-2710: Effect of combined linear and oscillatory acceleration on pilot attitude-control capabilities/by Constantine B. Dolkas and John D. Stewart |
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM |
Topical Term |
Hypersonic Ceramic-Heated |
653 ## - INDEX TERM--UNCONTROLLED |
Uncontrolled term |
Pilots Evaluation--NASA |
-- |
Pilots Evaluation--NASA |
700 ## - ADDED ENTRY--PERSONAL NAME |
Personal name |
Rolls, L. Stewart |
-- |
Drinkwater III, Fred J. |
-- |
Innis, Robert C. |
-- |
Reeder, John P. |
-- |
Clark, Louis E. |
-- |
Wilson, R. Gale |
-- |
Nixon, Charles W. |
-- |
Hubbard, Harvey H. |
-- |
Allen, Jerry M. |
-- |
Czarnecki, K. R. |
-- |
Moul, Martin T. |
-- |
Schy, Albert A. |
-- |
Whitehead, Allen H. |
-- |
Dunavant, James C. |
-- |
Corlett, William A. and |
-- |
Richardson, Celia S. |
-- |
Dolkas, Constantine B. |
-- |
Stewart, John D. |
942 ## - ADDED ENTRY ELEMENTS (KOHA) |
Koha item type |
Books |