Invention Grant
US6164596A Designs of and methodology for inward or outward, and partially inward
or outward turning flow hypersonic air-breathing and
rocket-based-combined-cycle vehicles
失效
向内或向外以及部分向内或向外转向超音速空气呼吸和基于火箭的联合循环车辆的设计和方法
- Patent Title: Designs of and methodology for inward or outward, and partially inward or outward turning flow hypersonic air-breathing and rocket-based-combined-cycle vehicles
- Patent Title (中): 向内或向外以及部分向内或向外转向超音速空气呼吸和基于火箭的联合循环车辆的设计和方法
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Application No.: US48080Application Date: 1998-03-25
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Publication No.: US6164596APublication Date: 2000-12-26
- Inventor: Ajay P. Kothari
- Applicant: Ajay P. Kothari
- Main IPC: B64C3/10
- IPC: B64C3/10 ; B64C30/00 ; B64G1/14 ; F02K7/10 ; B64G1/00
Abstract:
The present invention is a novel method of designing a space vehicle. Unlike all previous known methods of designing a space vehicle, the present invention relies upon Radial Deviation Parameter to devise the flow field which provides the aero-dynamic effect as well as serving as an energy source to propel the space vehicle. The present invention would provide a single stage to orbit vehicle, which is a noted advancement over the conventional multi-stage to orbit vehicle. Furthermore, the teaching of the Radial Deviation Parameter design method can also be applied to trans-continent flight vehicles.
Public/Granted literature
- USD377672S Exercise cycle Public/Granted day:1997-01-28
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