Accession Number : AD0452641


Title :   ESTIMATED PERFORMANCE REPORT FOR THE ADVANCED X-15A-2 AIRPLANE WITH ONE YLR-99-RM-1 ENGINE NAA MODEL NO. NA-240-2.


Descriptive Note : Rept. for Apr-Jun 64,


Corporate Author : NORTH AMERICAN AVIATION INC LOS ANGELES CA


Personal Author(s) : Tweedie, A F


Report Date : 09 Jul 1964


Pagination or Media Count : 65


Abstract : The pertinent exit and reentry performance of the Advanced X-15A-2 is presented in this report. The estimated maximum velocity for the contractor responsible overweight configuration is 8280 fps while in the probable flight configuration a maximum velocity of 7850 fps can be achieved. (Author)


Descriptors :   *ROCKET AIRCRAFT , PERFORMANCE(ENGINEERING) , ASCENT TRAJECTORIES , ATMOSPHERE ENTRY , VELOCITY , WEIGHT , TABLES(DATA) , RESEARCH AIRCRAFT , LIQUID PROPELLANT ROCKET ENGINES


Distribution Statement : APPROVED FOR PUBLIC RELEASE