STAROVEROV'S SPACECRAFT (VERSIONS) AND/OR ALGORITHMS OF ITS OPERATION Russian patent published in 2014 - IPC B64G1/14 

FIELD: transport.

SUBSTANCE: invention relates to aerospace engineering. Spacecraft comprises two stages with wings, ramjet engines, center wing section, front horizontal fins, hook for vertical landing, cargo hatch, stage separation interlocking, retractable keels, rocket booster, jettisonable frames and cowlings. Rocket booster propellant comprises the following components. i.e. beryllium boranes, ammonium dinitramide and beryllium. Spacecraft is launched vertically to wing efficiency velocity and turned and brought to altitude of trust-to-weight ratio reduction, accelerated to velocity of ramjet engine efficiency, afterburning mode is actuated to separate second stage with rocket booster and to change over to horizontal path, second stage engines are actuated to land first and second stages.

EFFECT: increased payload.

22 cl, 4 dwg