Matches 1 - 16 out of 16

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US20110180670 In orbit space transportation & recovery system  
An In Orbit Transportation & Recovery System (IOSTAR™) (10) is disclosed. One preferred embodiment of the present invention comprises a space tug powered by a nuclear reactor (19). The IOSTAR™...
US20140263842 Reusable Global Launcher  
A reusable unmanned single-stage boost-glide suborbital Earth launcher, able to propel large or smaller payloads from Earth surface or from air launch, to a nearly Earth-orbital condition, then...
US20140124626 SPACE SHUTTLE PROGRAM ORBITAL VEHICLE COMPRISING A MULTIPLE PASSENGER BAY MODULE  
The application provides a Space Shuttle Program (SSP) Orbital vehicle comprising a payload bay comprising a pressure vessel comprising a passenger bay module adapted to provide and maintain...
US20110042521 Spacecraft Launch and Exploration System  
This invention is a launch-to-space, refuel and return system which comprises: a unique circular and straight maglev track and maglev sled spacecraft launcher; a single stage-to-LEO spacecraft...
US20100314498 Personal spacecraft  
The spacecraft structure is provide, the spacecraft structure for the spacecraft includes, a center fuselage, right wing side fuselage, left wing side fuselage, front wings, and rear wings of...
US20080111030 Process for recoving a launch vehicle first stage  
The invention is a process for returning the first stage booster of a launch vehicle having at least one upper stage, the first stage booster having a rocket engine system and aerodynamic flight...
US20050279889 Variable wing spacecraft  
A spacecraft having a fuselage, a severely swept back fixed wing and an extendible wing panel is disclosed. The extendible wing panel is rotatably extended after reentry into the atmosphere and is...
US20140124627 COMMERCIALLY FEASIBLE METHOD OF FLYING REPEATED ORBITAL MISSIONS USING A SPACE SHUTTLE PROGRAM ORBITAL VEHICLE  
The application provides a commercially feasible method of flying repeated orbital missions using a Space Shuttle Program (SSP) Orbital Vehicle.
US20130007935 Rocket Launch System and Supporting Apparatus  
A rocket launch system (1) includes a tubular rocket launcher carriage (2) with electromotive cableway traction drives (26) conveyed beneath a two axis pivot (63) anchored to the earth, elevated...
US20090140101 Direct Flight Far Space Shuttle  
A vehicle and method for enabling propulsive flight from suborbital altitudes and velocities directly to far space, or beyond Low Earth Orbit (LEO), preferably without requiring injection into or...
US20090173830 Rocket-powered kite plane for gentle climb and acceleration to extreme staging altitudes  
A two-stage space vehicle is provided for achieving low earth orbit that includes a carrier and an orbiter. The carrier has a large airfoil area relative to its dry weight, and the thrust of the...
US20140014779 Direct Flight Far Space Shuttle  
A vehicle and method for enabling propulsive flight from suborbital altitudes and velocities directly to far space, or beyond Low Earth Orbit (LEO), preferably without requiring injection into or...
US20170129626 LEO LB-1A SATELLITE LAUNCH SYSTEM  
The present invention, LB-1A, is a system for launching satellites, including small-sats, mini-sats, nano-sats, medical and scientific experiments, sub-orbital, orbital, and other aerospace...
US20160347480 AIRCRAFT CAPABLE OF PASSING FROM THE AERIAL DOMAIN TO THE SPATIAL DOMAIN AND METHOD FOR AUTOMATICALLY ADAPTING THE CONFIGURATION OF SAME  
An aircraft is capable of passing from the aerial domain to the spatial domain and method for automatically adapting the configuration of same. An additional breathable gas supply is provided to...
US20160244188 Trans-orbital freight and passenger carrier apparatuses supporting trans-orbital pipeline operations  
This invention is pioneering a Strategic Trans-orbital Carrier (herein called ‘a carrier’) which merges the technologies attributes of a plurality commercial jet engines with a plurality reusable...
US20160052650 DEVICE FOR CONTROLLING THE SPEED OF A SPACEPLANE DURING THE TRANSITION FROM A PHASE OF SPACE FLIGHT TO A PHASE OF AERONAUTICAL FLIGHT AND ASSOCIATED TRANSITION METHOD  
A spaceplane suitable for aeronautical flight comprising a body and a wing defining a lower airfoil surface in addition to attitude control means that comprise one or a plurality of shutters...
Matches 1 - 16 out of 16