000 00628nam a2200169 4500
005 20210105115100.0
008 210105b xxu||||| |||| 00| 0 eng d
040 _cIIT Kanpur
041 _aeng
100 _aDickmanns, E. D.
245 _aThe effect of finite thrust and heating constraints on the synergetic plane change maneuver for a space shuttle orbiter class vehicle [NASA Tn D-7211]
_cE. D. Dickmans
260 _aWashington, D. C.
_bNational Aeronautics and Space Administration
_c1973
300 _a38p
440 _aNational Aeronautics and Space Administration (NASA)
650 _aSpace shuttle
942 _cREF
999 _c563805
_d563805