000 00725nam a2200205 4500
003 OSt
005 20230110120854.0
008 230110b xxu||||| |||| 00| 0 eng d
040 _cIIT Kanpur
041 _aeng
100 _aWanhainen, John P.
245 _aEffect of injection element radial distribution and chamber geometry on acoustic mode instability in a hydrogen oxygen rocket [NASA TN D-5375]
_cJohn P. Wanhainen
260 _aWashington, D. C.
_bNational Aeronautics and Space Administration
_c1969
300 _a43p
440 _aNational Aeronautics and Space Administration
440 _aNASA Technical Note
500 _aBound vol. contains NASA TN D 5371-5380
650 _aOxygen rocket
942 _cTR
999 _c566392
_d566392