US 5,664,742 AGranted

Plume avoidance maneuvers

AssigneeThe United States of America as represented by the Secretary of the Navy

InventorWilliam J. Mason

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Abstract

A maneuver for minimizing perturbations on a released re-entry body due to ases exhausted from the nozzles of the post-boost control system in which after release of the re-entry body from a position compatible accomplishing with the maneuver, a flip turn is initiated in a near-nozzle-off configuration. The turn is preferably executed in a direction to the side of the direction of the velocity gain required for the platform to reach the next release location. The flip turn is stopped at a lateral escape angle, preferably after turning through an angle of 90 degrees or greater, by initiating an oppositely directed body-axis turn. After being accelerated for a lateral escape time, the platform is oriented in the direction of the required gain in velocity to reach the next release location and coarse thrust is activated. Prior to arrival at the release location, a body-axis turn is accomplished to orient the platform in the proper position for the next release event.

Claims7

Dependent claims

A method for minimizing perturbations on a released re-entry body released from an aerospace platform, which aerospace platform is moving in a generally ballistic path at a post-boost velocity, said aerospace platform bearing a plurality of releasable re-entry bodies mounted thereon, and said platform also having a fueled post-boost control system which includes a gas generator containing fuel and a plurality of nozzles for exhausting gases from the gas generator fuel to control the direction, orientation and velocity of said platform to achieve a desired pre-selected location for release of a releasable re-entry body, said perturbations on a released re-entry body being due to gases being exhausted from the nozzles of the post-boost control system of said aerospace platform during deployment of the platform to a desired pre-selected re-entry-body-release location for release of a releasable re-entry body, which method comprises:

(a) initiating a flip turn of said platform which is moving in a generally ballistic path at a post-boost velocity, said flip turn being in a first direction away from the direction required to reach said desired pre-selected re-entry-body-release location;
(b) stopping said flip turn after said platform has turned through a first predetermined angle;
(c) accelerating said platform in said first direction and at said predetermined angle to provide a lateral escape distance between the platform and the previously released re-entry body;
(d) turning said platform to establish a platform longitudinal axis orientation in the direction required to reach said desired pre-selected re-entry-body-release location;
(e) accelerating said platform to provide the required velocity to reach said desired pre-selected re-entry-body-release location;
(f) turning said platform to orient said platform in the proper orientation for release of said re-entry body.

3 more elements

A method for maneuvering an aerospace platform, said platform having a generally ballistic trajectory and bearing at least two releasable re-entry bodies thereon, said platform further having a fueled, post-boost control system of the type having four valve clusters, each valve cluster including two opposing high thrust nozzles oriented to provide oppositely directed thrust parallel to the platform's longitudinal axis, each valve cluster further including two opposing low thrust nozzles oriented to provide oppositely directed thrust in the plane normal to the platform's longitudinal axis and thereby control the direction, orientation and velocity of said platform prior to and after releasing a re-entry body, said maneuver after releasing a re-entry body providing a velocity required to reach a desired pre-selected re-entry-body-release location while minimizing perturbations on the just-released re-entry body due to gases exhausted from the nozzles of the post-boost control system during deployment of the platform to another desired pre-selected re-entry-body-release location and at the same time minimizing the fuel required to accomplish the maneuver, which method comprises:

(a) initiating a flip turn of said platform in a first direction away from the direction of the velocity required to reach said another desired pre-selected re-entry-body location, said step of initiating a flip turn being accomplished by operating the nozzles nearest the just-released re-entry body in a near-nozzle-off configuration;
(b) stopping said flip turn after said platform has turned through a first predetermined angle;
(c) accelerating said platform in said first direction and at said predetermined angle to provide a lateral escape distance between the platform and the just-released re-entry body;
(d) turning said platform to establish a platform longitudinal axis orientation in the direction of the required velocity to reach the desired pre-selected next-re-entry-body location;
(e) accelerating said platform to provide the required velocity to reach the next desired pre-selected re-entry-body-release location;
and
(f) turning said platform to orient said platform in the proper orientation for release of the next re-entry body in the desired pre-selected location.

4 more elements

Dependencies are inferred from the claim text.