System and methods for integrating a payload with a launch vehicle

• US 6,845,949 B2
• Filed: 07/23/2002
• Issued: 01/25/2005
• Est. Priority Date: 07/23/2002
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Gale, Anita E., Blackwell-Thompson, Judith C., Graves, John A.
• Primary Examiner(s): DINH, TIEN QUANG
• Application Number:
  US10/201,620
• Publication Number:
  US 20040016852A1
• Time in Patent Office: 917 Days
• Field of Search: 244/158.R, 244/118.1, 244/161, 244/137.1
• US Class Current: 244/173.1
• CPC Class Codes: B64C 1/20 specially adapted for freight
• CPC Class Codes: B64D 9/00 Equipment for handling freight; Equipment for facilitating passenger embarkation or the like emergency equipment B64D17/00, B64D19/00, B64D25/00; structures integral with fuselage to facilitate loading, fuselage floors specially adapted for freight, steps mounted on and retractable within aircraft B64C; ground installations B64F
• CPC Class Codes: B64G 1/002 Launch systems
• CPC Class Codes: B64G 1/14 Space shuttles reusable launch rockets B64G1/006
• CPC Class Codes: B64G 1/641 Interstage or payload connectors docking systems B64G1/646

Abstract

A system for providing an interface between a launch vehicle and a payload of the launch vehicle includes payload integration points of the launch vehicle that remain unchanged relative to different payload configurations, such that a payload is configurable apart from the launch vehicle. The system makes it possible to de-couple payload installation and launch vehicle turnaround operations. Payloads can be configured off-line from launch vehicle processing, thus making it possible to accommodate unique payloads while reducing wear and tear on the launch vehicle.

Claims

1. An interface system for providing an interface between a launch vehicle and a payload of the launch vehicle, the interface system comprising a plurality of payload integration points of the launch vehicle which include mission specific information that remain unchanged relative to different payload configurations such that a payload is configurable apart from the launch vehicle;

and

wherein the interface system includes at least one interface element configurable to interface with the payload configuration to provide the payload configuration with mission specific information received from at least one of the launch vehicle payload integration points.

2. The interface system of claim 1 wherein the interface element is configurable with the payload apart from the launch vehicle.

3. The interface system of claim 1 wherein the integration points comprise an avionics interface.

4. The interface system of claim 3 wherein the avionics interface is located in a payload bay of the launch vehicle.

5. The interface system of claim 1 wherein the interface element comprises a payload carrier configured to interface with a payload integration point in a payload bay of the launch vehicle.

6. The interface system of claim 1 wherein the payload integration point is comprised by a vehicle software system and the interface element comprises a front-end software module configurable to include a payload-specific object.

7. The interface system of claim 1 further comprising a testing system for testing a payload configuration with respect to at least one of the payload integration points.

8. A system for integrating a payload with a launch vehicle, the system comprising:

a payload carrier in which the payload is assembled apart from the vehicle, the carrier configured to provide an interface between the payload and the vehicle; and

a plurality of standardized payload integration points of the vehicle;

wherein the payload carrier is further configured to interface with at least one of the payload integration points to receive mission specific information.

9. The system of claim 8 wherein the integration points comprise an avionics system interface, the payload carrier further configured to provide an avionics interface between the payload and the vehicle.