000 00523 a2200157 4500
005 20220926092909.0
100 _aBauer, Helmut F.
245 _aNASA TN [D-1831]
_bthe effect of porpellant sloshing on the stability of an accelerometer controlled rigid space vehicle
_cHelmut F. Bauer
260 _aWashington
_bNASA
_c1963
300 _a82p
440 _aNASA Technical Note
490 _aD-1831
500 _aTechnical Reports D-4681-90 Bound Vol. No.101100;Contents: TR10010-18
650 _aAerospace
942 _cTR
999 _c566168
_d566168