FIELD: aero-space engineering; construction of recoverable multi-mission aero-space aircraft-carriers and methods of injection of space objects into near-earth orbit by means of aircraft-carriers.
SUBSTANCE: proposed aircraft-carrier is constructed from separate components forming single complex which includes separable platform-landing gear used for horizontal takeoff from runway, jettisonable cell-type wing (in one version) for enhancing total aerodynamic property and separable aircraft-stages which are placed one on another locking subsequent stage on pylons of cargo deck of previous stage. After separation, aircraft carriers return to runway. Last (third in particular) aircraft-carrier is orbital carrier. In case aircraft is not provided with cell-type wing, wing of first aircraft carrier is made with adequate span and length of chord for performing initial stage of flight in aircraft mode. Then, recoverable aircraft-carrier smoothly changes aircraft trajectory by ascending line to ballistic section of injection trajectory. As a result, cell-type wing is jettisoned.
EFFECT: reduced usage of materials; low cost of injection of payload.
18 cl, 11 dwg
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Authors
Dates
2004-07-20—Published
2001-09-05—Filed