FIELD: transportation of payloads in Earth-orbit airway; interorbital services. SUBSTANCE: interorbital aerospace vehicle has subsonic acceleration aircraft 1, intermediate acceleration stage 3 and orbital aircraft 5. Acceleration aircraft 1 is provided with turbojet engine plant 2; intermediate acceleration stage 3 is provided with mixed power plant 4 which consists of ramjet engine and liquid-propellant rocket engine. Orbital aircraft 5 is mounted on fuselage of intermediate acceleration stage 3 for separation; stage 3 is mounted on fuselage of subsonic acceleration aircraft 1 for separation. EFFECT: enhanced reliability. 6 dwg
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