Satellite communication system, infrastructure and method of providing same

• US 20100327119A1
• Filed: 06/29/2010
• Published: 12/30/2010
• Est. Priority Date: 06/30/2009
• Status: Abandoned Application

• Current Assignee: U.S. Space, LLC
• Original Assignee: U.S. Space, LLC
• Inventors: Piegza, Mark J., HOROWITZ, Edward D.
• Application Number:
  US12/825,759
• Publication Number:
  US 20100327119A1
• Time in Patent Office: Days
• US Class Current: 244/173.1
• CPC Class Codes: B64G 1/1007 Communications satellites
• CPC Class Codes: H04B 7/18515 Transmission equipment in satellites or space-based relays
• CPC Class Codes: Y10T 29/49002 Electrical device making

Abstract

A satellite communication system, infrastructure, and method of providing same, involves inventorying certain types of pre-selected communication satellite payload modules and communication satellite bus modules based on analysis of anticipated communication satellite needs and providing each payload and bus module with a pre-configured standard interface coupling. When communication satellite parameters for a customer are received, a selection is made of one or more of the inventoried payload modules and also of the inventoried communication satellite bus module that is sized and configured to accommodate the selected payload module or modules. The selected payload module or modules are coupled to the selected bus module via the standard interface coupling, and the selected bus module is, in turn, coupled to a launch vehicle.

Claims

1. A communication satellite assembly, comprising:

at least one communication satellite payload module being selected according to pre-defined communication satellite parameters from an inventory of communication satellite payload modules consisting at least in part of three different types of communication satellite payload modules for three different communication satellite frequency band types, each of said inventoried communication satellite payload modules being provided with a pre-configured standard interface coupling;

one of a first and second size communication satellite bus module configured to accommodate said selected at least one inventoried communication satellite payload module and being selected according to said pre-defined communication satellite parameters from an inventory of communication satellite bus modules consisting at least in part of a plurality of a first size communication satellite bus modules configured to accommodate at least a first of said three different types of communication satellite payload modules and a plurality of a second size communication satellite bus modules configured to accommodate at least a second of said three different types of communication satellite payload modules, each of said inventoried communication satellite bus modules being provided with said pre-configured standard interface coupling;

said at least one selected communication satellite payload module being coupled to said selected communication satellite bus module via said pre-configured standard interface coupling; and

said selected communication satellite bus module being coupled to a communication satellite launch vehicle.

2. The communication satellite assembly of claim 1, wherein said pre-defined communication satellite parameters comprise orbit and frequency band parameters compatible with a terrestrial infrastructure used by a governmental entity.

3. The communication satellite assembly of claim 1, wherein each of said inventoried communication satellite payload modules comprises one or more antennas, amplifiers and transponders.

4. The communication satellite assembly of claim 1, wherein said three different types of communication satellite payload modules further comprise communication satellite payload module types for each of at least three different communication satellite frequency band types consisting of one or more wideband frequency payload types, one or more narrow band frequency payload types, and a combination of one or more wideband and one or more narrow band frequency payload types.

5. The communication satellite assembly of claim 1, wherein each of said inventoried communication satellite bus modules comprises a structural sub-system, a telemetry sub-system, power sub-systems, a thermal control sub-system, and an attitude and orbit sub-system.

6. The communication satellite assembly of claim 1, wherein one size of said first and second size communication satellite bus modules is configured to accommodate at least one communication satellite payload module for either a communication satellite wideband frequency type payload or a communication satellite narrow band frequency type payload and the other size of said first and second size communication satellite bus modules is configured to accommodate at least one communication satellite payload module for each of a communication satellite wideband frequency type and a communication satellite narrow band frequency type.

7. The communication satellite assembly of claim 1, further comprising a communication satellite bus control device for managing the communication satellite bus module and a communication satellite payload module control device for managing the communication satellite payload module, both of said control devices being deployed to a communication satellite customer for exclusive management control of said selected communication satellite bus and payload modules.

8. The communication satellite assembly of claim 7, wherein said communication satellite bus control device comprises a first computing device in wireless communication with the selected communication satellite bus module and wherein said communication satellite payload control device comprises a second computing device in wireless communication with the selected communication satellite payload module.

9. The communication satellite assembly of claim 1, further comprising at least one video camera mounted on an exterior of said selected communication satellite bus module for providing a real time view of an environment surrounding said selected communication satellite bus module.

10. The communication satellite assembly of claim 1, wherein selected said communication satellite bus module further comprises at least one refueling valve allowing direct access to a satellite fuel tank for refueling.

11. The communication satellite assembly of claim 10, wherein said at least one refueling valve further comprises a locking mechanism to prevent inadvertent or unauthorized access to the satellite fuel tank.

12. A method of making a communication satellite assembly, comprising:

analyzing, using a computer, data consisting at least in part of historical data regarding usage of communication satellite payload types to identify anticipated deployment needs for at least three different communication satellite frequency band types;

inventorying a plurality of communication satellite payload modules consisting at least in part of three different types of communication satellite payload modules for said at least three different communication satellite frequency band types;

inventorying a plurality of communication satellite bus modules consisting at least in part of a plurality of a first size communication satellite bus module configured to accommodate at least a first of said three different types of communication satellite payload module and a plurality of a second size communication satellite bus module configured to accommodate at least a second of said three different types of communication satellite payload modules;

providing each of said inventoried communication satellite payload modules and each of said inventoried communication satellite bus modules with a pre-configured standard interface coupling;

selecting according to pre-defined communication satellite parameters at least one of said inventoried communication satellite payload modules;

selecting according to said pre-defined communication satellite parameters one of said first and second size communication satellite bus modules configured to accommodate said selected at least one inventoried communication satellite payload module;

coupling said selected communication satellite payload modules to said selected communication satellite bus module via said pre-configured standard interface coupling; and

coupling said selected communication satellite bus module to a communication satellite launch vehicle.