Single stage to orbit spacecraft
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Description
FIG. 1 is a perspective view of the aircraft;
FIG. 2 is a side view of the aircraft;
FIG. 3 is a top view of the aircraft;
FIG. 4 is a front view of the aircraft;
FIG. 5 is a bottom view of the aircraft; and,
FIG. 6 is a back view of the aircraft.
Referenced Cited
U.S. Patent Documents
D220985 | June 1971 | Webb |
D362234 | September 12, 1995 | Urie, Jr. |
3743218 | July 1973 | Sweeney et al. |
Patent History
Patent number: D396685
Type: Grant
Filed: Aug 5, 1996
Date of Patent: Aug 4, 1998
Assignee: Lockheed Martin Corporation
Inventors: Robert I. Baumgartner (Newhall, CA), John D. Elvin (Santa Clarita, CA), Jordan S. Reaser (Pacific Palisades, CA)
Primary Examiner: Kay H. Chin
Attorney: Robert A. Schruhl
Application Number: 0/57,944
Type: Grant
Filed: Aug 5, 1996
Date of Patent: Aug 4, 1998
Assignee: Lockheed Martin Corporation
Inventors: Robert I. Baumgartner (Newhall, CA), John D. Elvin (Santa Clarita, CA), Jordan S. Reaser (Pacific Palisades, CA)
Primary Examiner: Kay H. Chin
Attorney: Robert A. Schruhl
Application Number: 0/57,944
Classifications
Current U.S. Class:
Space Satellite Or Habitat (7) (D12/320);
Horizontal Stabilizer Conforms To And Continues Wing Or Fuselage Configuration, E.g., Lifting Body Type (D12/333)
International Classification: 1207;
International Classification: 1207;