000			00425pam a2200145a 44500
082			_aNASA _bMEMO 4-21-59E -
100			_aKrebs,Richard P
245	1		_aANALYSIS OF FLOW-SYSTEM STARTING DYNAMICS OF TURBOPUMP-FED LIQUID-PROPELLANT ROCKET
260			_a _bNasa, Washington, D.C. _c1959
300			_a45
500			_aBound With Nasa Memo 4-6-59e-4-30-59e
700			_aHart,Clint E
964			_gCIRC
997			_aTR7710 C
999			_c393925 _d393925