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Reusable orbital vehicle with interchangeable cargo modules

a technology of cargo modules and orbital vehicles, applied in the field of rockets, can solve the problems of large external fuel tanks burning up on re-entry, not being recycled, and being expensive to launch and operate, and being unable to meet the needs of space shuttles,

Inactive Publication Date: 2007-03-22
KISTLER AEROSPACE CORP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The large external fuel tank burns up on re-entry and is not recycled.
Even with the reusable portions of the space shuttle, the launch cost and operational cost of the space shuttle is significant.
Virtually all satellites, such as communications satellites, weather satellites, and the like, are currently launched on expensive, expendable launch vehicles that are discarded after placing their payloads into orbit.
Despite the recycling of some components, those skilled in the art will appreciate that the operation of the space shuttle presents a significant cost burden.

Method used

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  • Reusable orbital vehicle with interchangeable cargo modules
  • Reusable orbital vehicle with interchangeable cargo modules
  • Reusable orbital vehicle with interchangeable cargo modules

Examples

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Embodiment Construction

[0028] A reusable cargo module having selected standardized dimensions is designed to fit atop a reusable orbital vehicle to provide low cost delivery and retrieval of cargo into orbit. Although other suitable launch vehicles are possible, the reusable space launch vehicle 100, shown in FIG. 1, may be satisfactorily implemented by the Kistler K-1 vehicle. The space launch vehicle 100 comprises a launch assist platform (LAP) 102, which is sometimes referred to as a booster rocket. An orbital vehicle (OV) 104 is mounted atop the LAP 102. The Kistler K-1 vehicle utilizes three LAP engines 106. Fuel is supplied to the LAP engines 106 from LAP fuel tanks 108. In a typical implementation, separate fuel tanks contain rocket propellant and liquid oxygen (LOX). Operation of the LAP engines 106 and LAP fuel tanks 108 is known to one skilled in the art and need not be described in greater detail herein. The LAP 102 also contains avionics hardware, such as a vehicle computer, GPS, guidance syst...

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Abstract

A reusable module is affixed atop a reusable orbital vehicle (OV). Various configurations of the reusable module have identical external dimensions in the region of attachment to the OV to permit interchangeability. Different configurations can accommodate a variety of missions of different type and duration. A variety of cargo modules of different configurations allow cargo to be uplifted into orbit. In one embodiment, the cargo module is an unpressurized cargo module in which the cargo is exposed to the environment of space during the unloading process. The cargo module may also be a pressurized cargo module. In an alternative embodiment, the cargo module may include both a pressurized cargo module and unpressurized cargo module.

Description

BACKGROUND OF THE INVENTION [0001] 1. Field of the Invention [0002] The present invention is directed generally to rockets, and, more particularly, to a reusable orbital vehicle and reusable cargo module. [0003] 2. Description of the Related Art [0004] The modern space age may be thought of as beginning on Oct. 4, 1957 with the launch of Sputnik I. From that time until the launch of the first space shuttle in 1981, all portions of the space vehicle were expendable. That is, no parts were reused in subsequent missions. [0005] With the advent of the space shuttle, the solid rocket boosters and orbital vehicle itself were recycled for use in subsequent missions. The large external fuel tank burns up on re-entry and is not recycled. Even with the reusable portions of the space shuttle, the launch cost and operational cost of the space shuttle is significant. [0006] Virtually all satellites, such as communications satellites, weather satellites, and the like, are currently launched on ex...

Claims

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Application Information

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Patent Type & Authority Applications(United States)
IPC IPC(8): B64G1/00F03H99/00
CPCB64G2001/1092B64G1/14B64G1/223
Inventor MUELLER, GEORGE E.KOHRS, RICHARD H.DUNCAN, WILLIAM B.COCHRAN, DAVID B.MISTEREK, DEAN L.BURLISON, TERRILL L.CURTIS, RYAN M.JOHNSON, THOMASBAILEY, RICHARD A.LIMERICK, CHARLES D.
Owner KISTLER AEROSPACE CORP
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