000 00406 a2200133 4500
001 89115
082 _aPR 842
090 _c42063
_d42063
100 _aMuhammad Naeem
245 _aTo design a rocket nozzle study its heat transfer characteristics and then design a suitable cooling system for the nozzle
260 _aKarachi
_bNED
_c1983
300 _a105p.
_eKhalid Pervez
500 _aBE Project Reports
942 _aCAE NUST
_kPR 842
999 _c324188
_d324188