Add to ORKGA two-stage earth-to-orbit transport is disclosed which includes an orbiter vehicle and a pair of boosters, each having a deployable oblique wing located along a longitudinal axis of the booster. The wing is deployed in an oblique disposition in supersonic and hypersonic speeds, and disposed at 90 degree for subsonic speeds encountered during entry. The oblique wing is driven axially and rotated by means of a turret mounted on rails
The goal of this conceptual design was to devise a reusable, commercially viable, single-stage-to-or...
A conceptual design is presented for a carrier vehicle for an air launched space booster. This airpl...
This paper is based on a performance and economics study of a Mach two oblique flying wing transport...
A two-stage earth-to-orbit transport includes an orbiter vehicle and a pair of boosters, each having...
The system includes reusable turbojet propelled booster vehicles releasably connected to a reusable ...
A near-term technology launch system is described in which Space Shuttle main engines are used on a ...
Various types of twin strap-on boosters were evaluated by applying them to a core vehicle. The core ...
A method and apparatus for transportation between orbits are presented. A tanker orbit transfer vehi...
A conceptual design study of a two-stage-to-orbit vehicle is presented. Three configurations were in...
The object of this design class was to design an earth-to orbit vehicle to replace the present NASA ...
This procedure is distinguished by two beating wings which together describe, in space, a succession...
Two separate student design groups developed conceptual designs for a two-stage-to-orbit vehicle, wi...
An aircraft including a single fuselage having a main wing and a horizontal stabilizer airfoil pivot...
Significant performance benefits are realized via aerodynamic braking and/or aerodynamic maneuvering...
A heavy launch vehicle is discussed. The launch vehicle is comprised of an expendable, multi-contain...
The goal of this conceptual design was to devise a reusable, commercially viable, single-stage-to-or...
A conceptual design is presented for a carrier vehicle for an air launched space booster. This airpl...
This paper is based on a performance and economics study of a Mach two oblique flying wing transport...
A two-stage earth-to-orbit transport includes an orbiter vehicle and a pair of boosters, each having...
The system includes reusable turbojet propelled booster vehicles releasably connected to a reusable ...
A near-term technology launch system is described in which Space Shuttle main engines are used on a ...
Various types of twin strap-on boosters were evaluated by applying them to a core vehicle. The core ...
A method and apparatus for transportation between orbits are presented. A tanker orbit transfer vehi...
A conceptual design study of a two-stage-to-orbit vehicle is presented. Three configurations were in...
The object of this design class was to design an earth-to orbit vehicle to replace the present NASA ...
This procedure is distinguished by two beating wings which together describe, in space, a succession...
Two separate student design groups developed conceptual designs for a two-stage-to-orbit vehicle, wi...
An aircraft including a single fuselage having a main wing and a horizontal stabilizer airfoil pivot...
Significant performance benefits are realized via aerodynamic braking and/or aerodynamic maneuvering...
A heavy launch vehicle is discussed. The launch vehicle is comprised of an expendable, multi-contain...
The goal of this conceptual design was to devise a reusable, commercially viable, single-stage-to-or...
A conceptual design is presented for a carrier vehicle for an air launched space booster. This airpl...
This paper is based on a performance and economics study of a Mach two oblique flying wing transport...