Add to ORKGA two-stage earth-to-orbit transport includes an orbiter vehicle and a pair of boosters, each having a depolyable 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
This paper is based on a performance and economics study of a Mach two oblique flying wing transport...
A conceptual design is presented for a carrier vehicle for an air launched space booster. This airpl...
A study to improve the performance of the NASA two-stage-to-orbit vehicle was undertaken. The NASA c...
A two-stage earth-to-orbit transport is disclosed which includes an orbiter vehicle and a pair of bo...
The system includes reusable turbojet propelled booster vehicles releasably connected to a reusable ...
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 ...
Various types of twin strap-on boosters were evaluated by applying them to a core vehicle. The core ...
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...
A near-term technology launch system is described in which Space Shuttle main engines are used on a ...
The concept to use twin turbo-powered boosters for acceleration to supersonic staging speed followed...
A method and apparatus for transportation between orbits are presented. A tanker orbit transfer vehi...
The present invention is a space launch system and method to propel a payload bearing craft into ear...
Significant performance benefits are realized via aerodynamic braking and/or aerodynamic maneuvering...
This paper is based on a performance and economics study of a Mach two oblique flying wing transport...
A conceptual design is presented for a carrier vehicle for an air launched space booster. This airpl...
A study to improve the performance of the NASA two-stage-to-orbit vehicle was undertaken. The NASA c...
A two-stage earth-to-orbit transport is disclosed which includes an orbiter vehicle and a pair of bo...
The system includes reusable turbojet propelled booster vehicles releasably connected to a reusable ...
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 ...
Various types of twin strap-on boosters were evaluated by applying them to a core vehicle. The core ...
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...
A near-term technology launch system is described in which Space Shuttle main engines are used on a ...
The concept to use twin turbo-powered boosters for acceleration to supersonic staging speed followed...
A method and apparatus for transportation between orbits are presented. A tanker orbit transfer vehi...
The present invention is a space launch system and method to propel a payload bearing craft into ear...
Significant performance benefits are realized via aerodynamic braking and/or aerodynamic maneuvering...
This paper is based on a performance and economics study of a Mach two oblique flying wing transport...
A conceptual design is presented for a carrier vehicle for an air launched space booster. This airpl...
A study to improve the performance of the NASA two-stage-to-orbit vehicle was undertaken. The NASA c...