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Container cabin for orbital vehicle

a cargo cabin and orbital vehicle technology, applied in the field of air breathing hypersonic propulsion modules, can solve the problems of low orbital cost, unobtainable degree of operational flexibility and responsiveness, and limited intra-space maneuverability

Inactive Publication Date: 2004-02-05
REDDING FRED WHITNEY JR +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

(1) a military / NASA air-launched, manned and unmanned hypersonic aircraft for conducting needed research in hypersonic flight technologies for the Government and industry;
(2) a military / NASA air-launched, manned space vehicle for conducting needed research in orbital and transatmospheric flight; and
(3) very low cost to orbit, and an otherwise unobtainable degree of operational flexibility and responsiveness for the Space Cruiser 14 in commercial, military and NASA use.
Indeed, the Cruiser 14 and its uses are highly synergistic with launch vehicles and their payloads.
NASA's Space Transportation System (STS) or "Shuttle", while limited severely in its intraspace maneuverability, is such a space transportation system.

Method used

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  • Container cabin for orbital vehicle
  • Container cabin for orbital vehicle
  • Container cabin for orbital vehicle

Examples

Experimental program
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Effect test

Embodiment Construction

: (Circular orbits except GTO) Commercial 2-stage Delta 6920 Florida (ESMC) 1 crewmember 2050 nmi circular & recover (i = 28.7) (Cruiser propellant limited by Delta 6920 throw weight) 2 crew members 1950 nmi circular & recover (i = 28.7) Commercial 2-stage Delta 7920 at ESMC 1 crewmember 2900 nmi circular & recover (i = 28.7) 2 crewmember 2550 nmi circular & recover (i = 28.7) 1 or 2 crew members to geosynch. transfer orbit (GTO) Commercial Delta 6920 California (WSMC) polar orbit 1 crewmember 1000 nmi (Throw weight limited) 2 crewmember 950 nmi (Throw weight limited) Commercial Delta 7920 at WSMC polar orbit 1 crewmember 1825 nmi (Throw weight limited) 2 crewmember 1740 nmi (Throw weight limited) Commercial Delta 6920 WSMC Sun-synchronous (i = 98.7) 2 crewmember 725 nmi Commercial Delta 7920 WSMC Sun-synchronous (i = 98.7) 1 crewmember 1585 nmi 2 crewmember 1510 nmi Potential lowest cost launch system Air Launch Cruiser Vehicle (ALCV) with launch price goal of $1-2 Million. Interna...

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PUM

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Abstract

A method for developing and utilizing a Space Cruiser vehicle efficiently combines resources from relevant end users in industry and the military. The preferred vehicle has an elongated conical shell with an elliptical transverse cross section. The cabin of the vehicle preferably has a circular transverse cross section, leaving space between the cabin and the shell to store vehicle fuel. The cabin is insulated and capable of supporting occupants in a shirt-sleeve, air-breathing environment whether in the Earth's atmosphere or in outerspace. The vehicle is capable of being launched from conventional aircraft, and also being stored in and launched from a spaced shuttle or orbiting space station.

Description

[0001] This application is a divisional of application Ser. No. 09 / 893,496, filed June, 2001 and entitled "HYPERSONIC AND ORBITAL VEHICLES SYSTEM", which is a continuation of U.S. patent application Ser. No. 09 / 188,208, filed Nov. 10, 1998 (now U.S. Pat. No. 6,257,527). This application claims priority from prior U.S. Provisional Patent Applications serial Nos. 60 / 064,771, filed Nov. 10, 1997, 60 / 064,772, filed Nov. 10, 1997 and 60 / 064,769, filed Nov. 10, 1997. The entire disclosures in these applications are expressly incorporated herein by this reference.[0002] 1. Technical Field[0003] The present invention pertains to an air breathing hypersonic propulsion module (ABPM) that, when attached to a manned Space Cruiser vehicle, will revolutionize manned access to orbit in terms of low cost, operational flexibility and responsiveness. The invention also pertains to an effective development program for the ABPM and the Space Cruiser.[0004] 2. Discussion of Prior Art[0005] Discussed her...

Claims

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Application Information

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Patent Type & Authority Applications(United States)
IPC IPC(8): B64G1/00B64G1/12B64G1/14
CPCB64G1/005B64G1/14B64G1/12
Inventor REDDING, FRED WHITNEY JR.REDDING, MARY
Owner REDDING FRED WHITNEY JR
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