Flight/launch vehicle and method ...

Abstract | Drawing | Description | Claims

Abstract
An airship is disclosed that stores air and uses it in a propulsion system that requires oxygen. This allows the airship to travel above the atmosphere, where oxygen is not available. The airship maximizes known mature technologies such as the buoyancy of a lighter than air balloon and the aerodynamic lift and propulsion of an airplane, until the altitude renders these technologies ineffective. The modified airship uses the stored air to extend transportation operations above natural limits and permit high-speed travel beyond traditional atmospheric speeds. Entering the edge of space at high tangential velocity permits placement of payloads into orbit. Entering the edge of space at low tangential velocity presents opportunities for low energy plane changes in orbital inclination. The modified airship may also alter the aerodynamic shape as desired in flight. The airship takes off, leaves and re-enters the atmosphere and lands without specialized launch facilities or long landing...

Application number: 11/330,018
Publication number: US 2007/0205330 A1
Filing date: Jan 11, 2006
Inventor: Douglas Wayne Hubbard
Assignees: Hubbard Aerospace, LLC

U.S. Classification
244171100

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Claims

What is claimed is:

1. An Air-Breathing Lung Reusable Launch Vehicle comprising:

a flexible air envelope having the shape of a lifting body and capable of storing air collected during flight,

at least one air-breathing engine comprising a by-pass flow thrust diverter capable of diverting outside air into the flexible air envelope, and

at least one fuel tank holding a liquefied or liquid fuel.

2. The Air-Breathing Lung Reusable Launch Vehicle of claim 1 further comprising:

a rigid keel attached to the flexible air envelope in an airtight manner.

3. The Air-Breathing Lung Reusable Launch Vehicle of claim 2 wherein the rigid keel comprises:

a heat resistant nose located at the leading edge of the vehicle,

thrust vectoring flaps capable of directing thrust generated by the at least one air-breathing engine,

an air inlet capable of conveying outside air to the at least one engine,

at least one flexible lifting cell, and

wherein:

the pressure within the flexible air envelope remains higher than the pressure outside the vehicle at all times.

4. The Air-Breathing Lung Reusable Launch Vehicle of claim 2 wherein:

the rigid keel extends from the nose of the vehicle along the bottom of the vehicle for at least 60% of the length of the vehicle.

5. The Air-Breathing Lung Reusable Launch Vehicle of claim 3 wherein:

the fuel is liquefied hydrogen and the lifting gas is hydrogen gas.

6. A method of achieving transatmospheric flight comprising:

storing air in a flexible air envelope during atmospheric flight for subsequent use as an oxidizer by air breathing engines above the atmosphere.

7. The method of claim 6 wherein air is diverted into the flexible air envelope by at least air-breathing engine comprising a by-pass flow thrust diverter capable of diverting outside air into the flexible air envelope.

8. The method of claim 7 wherein the airship comprises flexible lifting cells that can be filled with a lifting gas.

9. The method of claim 8 wherein lifting cells are situated within the flexible air envelope and, as the lung fills with air, lifting gas is vented from the lifting cells.

10. The method of claim 6 wherein the lung comprises a flexible air envelope attached to a rigid keel in an airtight manner to form a lifting body.