X-15 Advanced Research Airplane [NA-55-221] -

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Research and Development in Intelligent Systems XVIII: Proceedings of ES2001, the Twenty-first SGES International Conference on Knowledge Based Systems and Applied Artificial Intelligence, Cambridge, December 2001

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Additional resources for X-15 Advanced Research Airplane [NA-55-221] -

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228 LB LAUNCHING WEIGHT 27,684 LB BURN-OUT WEIGHT 10,405 LB STRUCTURAL DESIGN. 33G).. . . . . .. 10,443 LB 46 . I... I NA-55-221 . DESIGN MISSION . . - 250 0 0 0 two place version DESIGN PROFILE PULL UP 200 1 POWERED CLIMB TO BURNOUT, 150 § I CL=O - HIGH TEMPERATURE PROFILE PULL UP CLIMB TO 75, 000 FT -2 G PUSHOVER POWEROFF CLIMB TO POWEROFF MAX. ALTITUDE, CL MAX. 75 ~ DESCENT TO la, 000 FT OPT. GLIDE DESCENT TO la, 000 FT. OPT. GLIDE - --- 100 --- LEVELFLIGHT 50 « 0 100 0 200 300 400 TIME 7000 ~ 6000 ~~ 5000 ~ 4000 Q 3000 2000 ~ P4 U) " - 1000 o ,/ o I I I '" , - , 500 FROM I 600 - LAUNCH 800 900 T !

100 - 700 800 SECONDS 200 300 - 400 500 600 700 800 TIME FROM LAUNCH - SECONDS 900 1000 1100 1200 28 . c. I NA-55-221 DESIGN MISSIONS . · .. temperature V5. ' 1200 ,- - -- ......... ,... - I Z . I 400 I / '/ 1/ / I 200 AY -200 o 50 / /1 ,-' I MISSION DESIGN MISSION 100 / ..... 12 SKIN THICKNESS ---.... -..... -- --- ..... , ---..... ... 06 SKIN THICKNESS , r:USELAGE STATION100, BOTTOM I '-- WING . LOWERSURFACE25'10CHORD 08 SKIN THICKNESS \. '.. I 600 TEMPERATURE FUSELAGE STATION150, BOTTOM .

5 minutes. Three attempted engine restarts will extend over a period of 1 minute. At this time an altitude of 30,000feet has been reached. If it is assumed that all propellants are jettisoned by the time the 10,000 foot limit is reached, then the jettisoning procedure must begin at 16,000 feet. In the event the pilot is required to bail out, the normal procedure will be to use the ejection seat. The design dynamic pressures encountered are not higher than those assumed for present-day high performance aircraft, so the pilot in his seat should be able to clear the aircraft satisfactorily at any altitude.

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