US4504031A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Aerodynamic braking and recovery method for a space vehicle
Assignee: Boeing Co
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Filing: 1982-03-02
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Granted: 1985-03-12
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Expires: 2002-03-02
Abstract
Abstract A space vehicle 10 is steered from outer space toward the earth's atmosphere main rocket nozzle end first. An inflatable braking member 28 is deployed around the vehicle 10 by introducing gas into it. The main rocket motor 16 is ignited to produce a substantially throttled stream of gases. This stream provides a cooling layer forwardly of the braking member 28 to protect the member 28 from heating by friction with the atmosphere. The reduction of the velocity of the vehicle 10 is controlled by directly varying the drag of the vehicle 10 to compensate for variations in the density of the atmosphere. The drag is varied by varying the thrust of the motor 16 and/or varying the shape of the member 28. A backup method is to deflate the member 28 in the atmosphere. The member 28 may be jettisoned after the vehicle 10 leaves the atmosphere to enter a low earth orbit.
Inventors
- 👤 Dana G. Andrews
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-06 17:16
CPC Classifications
B; B64; B64G; B64G1/00; B64G1/22; B64G1/52; B64G1/58; B64G1/62; B64G1/623
Claims Analysis
Total Claims: 21
Claim 1
Independent Claim
173 words
A method of recovering a space vehicle for reuse, comprising: steering such space vehicle while it is in outer space, beyond a low earth orbit, for directing the space vehicle into a return path towards the earth's atmosphere, including orienting the space vehicle so that it will enter the earth's atmosphere main rocket nozzle end first; extending an aerodynamic braking member that is carried by such space vehicle from a stowed position out into a large drag operational position in which it presents a large area braking surface which extends generally laterally outwardly from the space vehicle; and operating the main rocket motor of the space vehicle to produce gases, regulating the flow rate of such gases out through the main rocket nozzle, so that the gases will flow back and outwardly to provide a cooling layer forwardly of the braking surface but without a substantial reduction in drag, whereby the braking surface will remain effective and the braking member will reduce the velocity of the space vehicle down to a desired level.
Claim 2
Independent Claim
173 words
A method of recovering a space vehicle for reuse, comprising: steering such space vehicle while it is in outer space, beyond a low earth orbit, for directing the space vehicle into a return path towards the earth's atmosphere, including orienting the space vehicle so that it will enter the earth's atmosphere main rocket nozzle end first; extending an aerodynamic braking member that is carried by such space vehicle from a stowed position out into a large drag operational position in which it presents a large area braking surface which extends generally laterally outwardly from the space vehicle; and operating the main rocket motor of the space vehicle to produce gases, regulating the flow rate of such gases out through the main rocket nozzle, so that the gases will flow back and outwardly to provide a cooling layer forwardly of the braking surface but without a substantial reduction in drag, whereby the braking surface will remain effective and the braking member will reduce the velocity of the space vehicle down to a desired level.
Claim 3
Dependent Claim
40 words
A method according to claim 1, comprising using an inflatable aerodynamic braking member, and moving such member from its stowed position to its operational position by introducing an inflation gas into it, from a source stored aboard the space vehicle.
Claim 4
Dependent Claim
49 words
A method according to claim 2, comprising utilizing a fuel composition for the main rocket motor which is stored aboard the space vehicle in a liquid state for inflating said aerodynamic braking member, by introducing some of such fuel composition into the inflatable braking member in a gaseous state.
Claim 5
Dependent Claim
97 words
A method according to claim 1, comprising combining liquid oxygen and liquid hydrogen in said rocket motor, for producing a high velocity gas stream to provide thrust during periods of such rocket motor use for propelling the space vehicle, and for producing a substantially throttled stream of gases when the space vehicle is being recovered and the aerodynamic braking member is operational, for providing a layer of gases over the anterior surface of the aerodynamic braking member, to shield such braking member against destructive heating by friction during reentry of the space vehicle into the earth's atmosphere.
Claim 6
Dependent Claim
33 words
A method according to claim 1, comprising jettisoning the aerodynamic braking member from the space vehicle after it has performed its function and the space vehicle has slowed down to a desired velocity.
Claim 7
Dependent Claim
36 words
A method according to claim 5, comprising operating the main rocket motor and directional rockets aboard the space vehicle for placing the space vehicle into a low earth orbit following jettisoning of the aerodynamic braking member.
Claim 8
Independent Claim
190 words
A method of recovering a space vehicle for reuse, comprising: steering such space vehicle while it is in outer space, beyond a low earth orbit, for directing the space vehicle into a return path towards the earth's atmosphere, including orienting the space vehicle so that it will enter the earth's atmosphere main rocket nozzle end first; extending an aerodynamic braking member that is carried by such space vehicle from a stowed position out into a large drag operational position in which it presents a large area braking surface which extends generally laterally outwardly from the space vehicle; operating the main rocket motor of the space vehicle to produce gases, including regulating the flow rate of such gases out through the main rocket nozzle so that the gases will flow back and outwardly to provide a cooling layer forwardly of the braking surface; and while so operating said rocket motor, taking steps for varying the drag of the space vehicle to correct for navigational errors and variations in the density of the atmosphere so that the braking member will reduce the velocity of the space vehicle down to a desired level.
Claim 9
Independent Claim
190 words
A method of recovering a space vehicle for reuse, comprising: steering such space vehicle while it is in outer space, beyond a low earth orbit, for directing the space vehicle into a return path towards the earth's atmosphere, including orienting the space vehicle so that it will enter the earth's atmosphere main rocket nozzle end first; extending an aerodynamic braking member that is carried by such space vehicle from a stowed position out into a large drag operational position in which it presents a large area braking surface which extends generally laterally outwardly from the space vehicle; operating the main rocket motor of the space vehicle to produce gases, including regulating the flow rate of such gases out through the main rocket nozzle so that the gases will flow back and outwardly to provide a cooling layer forwardly of the braking surface; and while so operating said rocket motor, taking steps for varying the drag of the space vehicle to correct for navigational errors and variations in the density of the atmosphere so that the braking member will reduce the velocity of the space vehicle down to a desired level.
Claim 10
Dependent Claim
40 words
A method according to claim 7, comprising using a inflatable aerodynamic braking member, and moving such member from its stowed position to its operational position by introducing an inflation gas into it, from a source stored aboard the space vehicle.
Claim 11
Dependent Claim
84 words
A method according to claim 8, wherein the steps for varying the drag of the space vehicle comprise: keeping the thrust of the rocket motor constant; and at the same time, maintaining a preprogrammed internal pressure in the inflatable aerodynamic braking member to allow said member to change shape with variations in the density of the atmosphere and thereby automatically correct for such variations in density by varying the effective drag area of said member and, thus, varying the drag of the space vehicle.
Claim 12
Dependent Claim
83 words
A method according to claim 9, comprising: utilizing a fuel composition for the main rocket motor which is stored aboard the space vehicle in a liquid state for inflating said aerodynamic braking member, by introducing some of such fuel composition into the inflatable braking member in a gaseous state; and maintaining said preprogrammed internal pressure in said member by introducing more of such fuel composition into said member and venting said composition from said member, as necessary to maintain said preprogrammed internal pressure.
Claim 13
Dependent Claim
112 words
A method according to claim 8, further comprising: shutting off said rocket motor after the velocity of the space vehicle has been reduced to said desired level; allowing the inflatable aerodynamic braking member to gradually cool and deflate while allowing the space vehicle to leave the sensible atmosphere; releasing connections between the space vehicle and the braking member and operating the main rocket motor, to move the braking member toward said motor and clear directional rockets aboard the space vehicle; operating the directional rockets to orient the space vehicle for placement into a low earth orbit; and operating the main rocket motor for propelling the space vehicle into such low earth orbit.
Claim 14
Dependent Claim
33 words
A method according to claim 11, comprising jettisoning the braking member from the space vehicle during the operation of the main rocket motor for propelling the space vehicle into such low earth orbit.
Claim 15
Dependent Claim
49 words
A method according to claim 8, comprising utilizing a fuel composition for the main rocket motor which is stored aboard the space vehicle in a liquid state for inflating said aerodynamic braking member, by introducing some of such fuel composition into the inflatable braking member in a gaseous state.
Claim 16
Dependent Claim
94 words
A method according to claim 7, wherein the steps for varying the drag of the space vehicle comprise varying the thrust of said motor while so regulating the flow rate of such gases, to vary the flow field of such gases around the braking member for varying the drag of the braking surface and thereby varying the drag of the space vehicle, so that the velocity of the space vehicle will be reduced to the desired level and, at the same time, such gases will provide a cooling layer forwardly of the braking surface.
Claim 17
Dependent Claim
84 words
A method according to claim 14, comprising: using an inflatable aerodynamic braking member, and moving such member from its stowed position to its operational position by introducing an inflation gas into it from a source stored aboard the space vehicle; and keeping the shape of said braking member constant, when said member is in its operational position and is reducing the velocity of the space vehicle, by maintaining a constant ratio between the internal pressure in said member and the external stagnation point pressure.
Claim 18
Dependent Claim
81 words
A method according to claim 5, comprising: utilizing a fuel composition for the main rocket motor which is stored aboard the space vehicle in a liquid state for inflating said aerodynamic braking member, by introducing some of such fuel composition into the inflatable braking member in a gaseous state; and adjusting the internal pressure in said member by introducing more of such fuel composition into said member and venting said composition from said member, as necessary to maintain said constant ratio.
Claim 19
Dependent Claim
105 words
A method according to claim 14: comprising using an inflatable aerodynamic braking member, and moving such member from its stowed position to its operational position by introducing an inflation gas into it, from a source stored aboard the space vehicle; and wherein the steps for varying the drag of the space vehicle further comprise maintaining a preprogrammed internal pressure in said braking member to allow said member to change shape with variations in the density of the atmosphere and thereby automatically correct for such variations in density by varying the effective drag area of said member and, thus, varying the drag of the space vehicle.
Claim 20
Dependent Claim
117 words
A method according to claim 14, comprising combining liquid oxygen and liquid hydrogen in said rocket motor, for producing a high velocity gas stream to provide thrust during periods of such rocket motor use for propelling the space vehicle, and for producing a substantially throttled stream of gases when the space vehicle is being recovered and the aerodynamic braking member is operational, for providing a layer of gases over the anterior surface of the aerodynamic braking member to shield such braking member against destructive heating by friction with the earth's atmosphere and to vary to drag of the space vehicle so that the braking member will reduce the velocity of the space vehicle to the desired level.
Claim 21
Dependent Claim
86 words
A method according to claim 15, claim 9, or claim 17: wherein the steps for varying the drag of the space vehicle further comprise deflating the aerodynamic braking member after the velocity of the space vehicle has been reduced to said desired level, relying on the gases produced by the main rocket motor to provide a cooling layer to protect the space vehicle; and further comprising allowing the space vehicle to leave the sensible atmosphere after deflating said braking member; and shutting off said rocket motor.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1988-03-11 | 1988-09-10 | 1989-03-12 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1992-03-11 | 1992-09-10 | 1993-03-12 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1996-03-11 | 1996-09-10 | 1997-03-12 | $7700.00 | Window Closed / Lapsed |