Algorithm of Launched Vehicles Mass Calculation at the Early Stage of Designing
Keyword(s):
Launching mass of pilotless vehicle bounds with flight path. Required fuel mass depends from flight trajectory. Design calculation of vehicle mass and flight trajectory are in close bind. We suggest numerical algorithm of design calculation of vehicle flight mass and optimal characteristics of flight trajectory – initial flight-path angle and flight time to target.
2013 ◽
Vol 791-793
◽
pp. 1073-1076
Keyword(s):
2019 ◽
Vol 233
(12)
◽
pp. 4436-4446