000			00481pam a2200145a 44500
082			_aNASA _bTN D-7028
100			_aArnaiz,H H
245	1		_aVALIDATION OF THE GAS GENERATOR METHOD OF CALCULATING JET-ENGINE THRUST AND EVALUATION OF XB-70-1 AIRPLANE ENGINE PERFORMANCE AT GROUND STATIC CONDITIONS.
260			_a _bNasa, Washington, D.C. _c1970
300			_a43
500			_aBound With Nasa Tn D-7020-27.
700			_aSchweikhard,W G
964			_gCIRC
997			_aTR11119 C
999			_c397553 _d397553