| 000 -LEADER |
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| fixed length control field |
01707nam a22002897a 4500 |
| 003 - CONTROL NUMBER IDENTIFIER |
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| control field |
OSt |
| 005 - DATE AND TIME OF LATEST TRANSACTION |
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| control field |
20220823152931.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
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| fixed length control field |
220704b xxu||||| |||| 00| 0 eng d |
| 040 ## - CATALOGING SOURCE |
|---|
| Transcribing agency |
IIT Kanpur |
| 041 ## - LANGUAGE CODE |
|---|
| Language code of text/sound track or separate title |
eng |
| 100 ## - MAIN ENTRY--AUTHOR NAME |
|---|
| Personal name |
Mirels, Harold |
| 110 ## - MAIN ENTRY--CORPORATE NAME |
|---|
| Corporate name or jurisdiction name as entry element |
Washington: National Aeronautics and Space Administration |
| 245 ## - TITLE STATEMENT |
|---|
| Title |
NASA technical note: NASA MEMO 59E |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) |
|---|
| Place of publication |
Washington , D. C. |
| Name of publisher |
National Aeronautics and Space Administration |
| Year of publication |
1959 |
| 300 ## - PHYSICAL DESCRIPTION |
|---|
| Number of Pages |
49p |
| 440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE |
|---|
| Title |
National Aeronautics and Space Administration |
| 440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE |
|---|
| Title |
NASA Technical Note |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA MEMO 59E:Source distribution method for unsteady one dimensional flows with small mass momentum and heat addition and small area variation by Harold Mirels 49p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA MEMO 59E: Analytical investigation of the effect of turnbopump design on gross weight chatectristics of a hydrogen propelled nuclear rocket by Harold E. Rohlik 37p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA MEMO 59E: Experimental altitude performance of jp-4 fuel and liquid oxygen rocket engine with an area ratio of 48 by Anthony Fortini 27p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA MEMO 59E: Performance characteristics of flush and shielded auxiliary exits at mach numbers of 1.5 to 2.0 by Kaleel L. Abdalla 21p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA MEMO 59E: Human tolerance to rapidly applied accelerations a summary of the literature by A. Martin Eiband 91p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA MEMO 59E: Theoretical performance of liquid oxygen as a rocket propellant by Sanford Gordon 137p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA MEMO 59E: Effect of ozone addition on combustion efficiency of hydrogen liquid oxygen propellant in small rockets by Riley O. Miller 17p |
| 650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical Term |
One-dimensional flows |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) |
|---|
| Koha item type |
Technical Report |
