| 000 -LEADER |
|---|
| fixed length control field |
00870pam a2200229a 44500 |
| 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 |
| 110 ## - MAIN ENTRY--CORPORATE NAME |
|---|
| Corporate name or jurisdiction name as entry element |
Washington. National Aeronautics and Space Administration (NASA) |
| 245 1# - TITLE STATEMENT |
|---|
| Title |
NASA Technical Note [NASA TN D-6297]: An investigation of two variations of the gas generator method to calculate the thrust of the afterburning turbofan engines installed in an F111A airplane |
| Statement of responsibility, etc |
Frank W. Burcham |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) |
|---|
| Name of publisher |
NASA |
| Year of publication |
1971 |
| Place of publication |
Washington |
| 300 ## - PHYSICAL DESCRIPTION |
|---|
| Number of Pages |
29p |
| 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 |
Bound together NASA TN D-6290 to 6299 |
| 500 ## - GENERAL NOTE |
|---|
| General note |
Bound vol. Acc. No. 101242 contains Acc. No. TR11521 to TR11529 |
| 650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical Term |
Aircraft |
| 650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical Term |
Propulsion systems |
| 650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical Term |
Thurst measurement |
| 700 ## - ADDED ENTRY--PERSONAL NAME |
|---|
| Personal name |
Burcham, Frank W. |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) |
|---|
| Koha item type |
Books |
