Patent ID: 6068211
Filing Date: 2000-05-30
Classification: B64G

Abstract:
A method of earth orbit space transportation and return utilizing a reusable flyback satellite, comprising the steps of:a) positioning a reusable flyback satellite to a desired release point which provides the capability of said satellite to achieve a desired orbit as defined by inclination and ascending node of the first orbit, wherein said step of positioning said reusable flyback satellite to a desired release point, comprises the steps of:(i) cross range positioning said reusable flyback satellite to a desired first position being said ascending node of the first orbit via an airbreathing carrier aircraft, wherein said reusable flyback satellite, having accelerating and positioning means attached thereto, is detached from said carrier aircraft; and,(ii) accelerating said reusable flyback satellite to said desired release point via said accelerating and positioning means whereupon said reusable flyback satellite is releasable from said accelerating and positioning means;b) deploying said satellite at said release point;c) injecting said satellite into orbit and overflying the geographic area of interest on said first orbit and for up to three additional consecutive orbits;d) providing on-orbit function and services to a payload of said satellite; and,e) de-orbiting, re-entering and landing said satellite with airplane-like functionality and utility.