000 00500pam a2200157a 44500
008 160408b1967 xxu||||| |||| 00| 0 eng d
082 _a629.134354
_bEX71
100 _aRindal,Roald A.
245 1 _aEXPERIMENTAL AND THEORITICAL ANALYSIS OF ABLATIVE MATERIAL RESPONSE IN A LIQUID PROPELLANT ROCKET ENGINE
260 _a
_bAerotherm Corporation, California
_c1967
300 _axv,
650 _aAblation (Aerothermodynamics)
650 _aRocket Engines
964 _gCIRC
997 _aA77718 C
999 _c309056
_d309056