| 000 -LEADER |
|---|
| fixed length control field |
02772nam a22003017a 4500 |
| 003 - CONTROL NUMBER IDENTIFIER |
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| control field |
OSt |
| 040 ## - CATALOGING SOURCE |
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| Transcribing agency |
IIT Kanpur |
| 041 ## - LANGUAGE CODE |
|---|
| Language code of text/sound track or separate title |
eng |
| 110 ## - MAIN ENTRY--CORPORATE NAME |
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| Corporate name or jurisdiction name as entry element |
Washington. National Aeronautics and Space Administration (NASA). |
| 245 ## - TITLE STATEMENT |
|---|
| Title |
NASA Technical Note [D-3491-3500] |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) |
|---|
| Place of publication |
Washington |
| Name of publisher |
National Aeronautics and Space Administration (NASA) |
| Year of publication |
1971 |
| 440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE |
|---|
| Title |
National Aeronautics and Space Administration (NASA) |
| 440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE |
|---|
| Title |
NASA Technical Note. |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA Technical Note [D-3491]: Temperature control unit for sounding rocket applications/ by kerstin Fredga and Robert S. Lee |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA Technical Note [D-3492]: Approximation of reentry angles of attack for a spinning body from rate-gyro and accelerometer data/ by Charles H. Whitlock |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA Technical Note [D-3493]:Low-speed tests of 50 degree-swept parawings applied to a 0.17-scale model of a manned flight vehicle/ by Frank M. Bugg |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA Technical Note [D-3494]: Error detection and correction approach to the time decoding problem/ by A.M. Demmerle, T. J. Karras, and P. J. McCeney |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA Technical Note [D-3495]: Analysis of tailored-interface operation of shock tubes with helium-driven planetary gases/ by William J. Loubsky and John O. Reller |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA Technical Note [D-3496]: Gemini spacecraft parachute landing system/ by John Vincze |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA Technical Note [D-3497]: On the dynamics of capillaries and the existence of plasma flow in the pericapillary lymph space/ by John T. Howe and Yvonne S. Sheaffer |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA Technical Note [D-3498]: Flutter at mach 3 of thermally stressed panels and comparison with theory for panels with edge rotational restraint/ by John L. Shideler, Sidney C. Dixon, and Charles P. Shore |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA Technical Note [D-3499]: Dynamic-model study of planetary-entry configurations in the langley spin tunnel/ Peter J. Costigan |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA Technical Note [D-3500]: Supersonic flutter of flat rectangular orthotropic panels elastically restrained against edge rotation/ by Larry L. Erickson |
| 650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical Term |
Tension Shells |
| 653 ## - INDEX TERM--UNCONTROLLED |
|---|
| Uncontrolled term |
Sounding Rocket-- Experiments |
| -- |
Rate-Gyro and Accelerometer Data |
| -- |
Low-Speed Wind-Tunnel --Investigation |
| -- |
Time Decoding Problem |
| -- |
Tailored Operation -- Shock Tube |
| -- |
Gemini Landing System |
| -- |
Capillary Endothelium |
| -- |
Thermal Stress-- Effect |
| -- |
Langley Spin Tunnel |
| -- |
Supersonic Flutter |
| 700 ## - ADDED ENTRY--PERSONAL NAME |
|---|
| Personal name |
Fredga, kerstin |
| -- |
Lee, Robert S. |
| -- |
Whitlock, Charles H. |
| -- |
Bugg, Frank M. |
| -- |
Demmerle, A.M. |
| -- |
Karras, T. J. |
| -- |
McCeney, P. J. |
| -- |
Loubsky, William J. |
| -- |
Reller, John O. |
| -- |
Vincze, John |
| -- |
Howe, John T. |
| -- |
Sheaffer, Yvonne S. |
| -- |
Shideler, John L. |
| -- |
Dixon, Sidney C. |
| -- |
Shore, Charles P. |
| -- |
Costigan, Peter J. |
| -- |
Erickson, Larry L. |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) |
|---|
| Koha item type |
Books |
