U.S. patents available from 1976 to present.
U.S. patent applications available from 2005 to present.

Multiconfiguration reusable space transportation system

Patent 4834324 Issued on May 30, 1989. Estimated Expiration Date: Icon_subject July 10, 2006. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.

Patent References

3202381

3369771

3405891

3702688

3881671

3884435

Three stage rocket vehicle with parallel staging Patent #: 4451017
Issued on: 05/29/1984
Inventor: Marshall

Inventor

Application

No. 06/883979 filed on 07/10/1986

US Classes:

244/158.9, Reusable or returnable244/2, COMPOSITE AIRCRAFTD12/320Space satellite or habitat (7)

Examiners

Primary: Barefoot, Galen L.

Attorney, Agent or Firm

International Classes

B64G 1/14 (20060101)
B64G 1/00 (20060101)
B64G 1/64 (20060101)
B64G 1/40 (20060101)
B64G 1/22 (20060101)

Abstract

A space transporation system comprises several different modular units usable in a plurality of different configurations for different payloads and space missions. The units include a first stage unit for providing primary propulsive force during launch, a payload carrying unit, which may be an orbital vehicle or simple payload canister, and an auxiliary propulsion unit for providing additional power either during launch or space flight. The units are all demountably securable together, and preferably all include aerodymanic devices such as fixed or swing wings for a controlled return to Earth. The first stage unit can act either as a single-stage-to-orbit vehicle carrying internal or external payload, or as the first stage of a multiple stage launch configuration including a payload unit and auxiliary propulsion units.

Other References

  • Salkeld, "Single-Stage Shuttles for Ground Launch and Air Launch", Astronautics Aeronautics, Mar. 1974, pp. 52-63
  • NASA Contractor Report No. 66685 "A Study to Determine the Weight and Performance Characteristics of Variable Geometry Spacecraft" vol. 1-Summary GDC-DCB68-012, 12 Jul. 1968. Prepared by Ken S. Coward
  • NASA CR-946 "Dynamic Stability of Space Vehicles" vol. XII-"Reentry Vehicle Landing Ability and Control" by B.J. Kuchta, Issued 1968, pp. 43, 45
  • NASA CR-1545 "A Study to Determine the Flight Characteristics and Handling Qualities of Variable Geometry Spacecraft"-vol. 1 High L/D Concept With Single Pivot, Two Position Skewed Wing by B.J. Kuchta dated 1969, p. 35
  • Boeing Aerospace Company (Jul. 1983), "Shuttle Derived Cargo Launch Vehicle Concept Definition Study": Study Extension (Final Report), NAS8-34599, pp. 83, 89, 94 to 96
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