FIELD: rocket engineering. SUBSTANCE: invention may be used for launching of intercontinental ballistic missiles from aircraft. Rocked laid on platform is drawn with the aid of pilot parachute, by force of pilot parachute rocket is turned in pitching channel to position in which air current starts to run against rocket from side opposite to platform. Platform is separated from rocket and is taken away by means of pilot parachute. Rocket motors are started and rocket is stabilized on specified trajectory with the use of control elements. EFFECT: enhanced reliability of launching. 3 dwg
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Authors
Dates
1996-10-20—Published
1992-08-24—Filed