Purveyor of Proprietary Propulsive & Virtual Technologies

Double Expansion -- US Patent #4817892: The art of staging a tapered aerobody as a secondary expansion nozzle, such that during hypersonic flight, combustion may be sustained in such enlarged expansion volume whilst employing hydrocarbons/kerosene as principal propellant thru the atmospheric range.

Ducted Rockets -- US Patents #5191716/4817892: Devising an air breathing rocket/aperture such that ambient air may be employed in lieu of tanked oxygen from takeoff thru space. Ditto hydrocarbons.

Asonic Aerospike Protocol -- US Patent #6213431, 4/01: Utilising hydrocarbon fuels in lieu of tanked hydrogen as primary orbital means of propulsion: Vortex // boundary layer management, adaptive keys, thrust vectoring, hydrocarbon/dual fuelling, bell hybrids. The future has arrived. Welcome X333.

THE APOLLO MYTH - ORBITAL THRUST - BROADBAND ENIGMA
With the Apollo epic rapidly withering into a distant fable, man's next quest will most certainly entail the planetary system, prior to setting off into deep space. However, with orbital means prohibitively expensive and limited to an elitist pool, space travel is set to remain a distant myth.

The development of innovative propulsive/ shuttle technologies and support systems will hence dictate man's exploration into space -- with air breathing rockets, liquid air & spiked aerospikes* cues to the future.

Meanwhile the perfusion of the Internet proved least to mention sensational. However, barring the convenience of e-books, e-banking, e-bookings & e-burgers, surfing essentially remains the name of the game. With Broadband a nouveau perfunctory, suburbia remains locked in a bandwidth chasm -- with fiber deemed an elitist luxury. Eurns may well be likeable, but the real cues will be connectivity, diffusivity & symbiosis.

U-TURN
A reversible aerospace plane includes an air intake at a first end of the aerospace plane, at least one heat exchanger disposed in the aerospace plane, an engine at a second end of the aerospace plane, wherein the aerospace plane is configured to accelerate in a first direction and configured to glide and land in a second direction, wherein the second direction is substantially in a reverse direction from the first direction.