Granted Patent B2

US 12,246,855 · App. 17/549,613 · Granted Mar 11, 2025

Inventor: Lyon B. King (Houghton, MI)

Assignees: MICHIGAN TECHNOLOGICAL UNIVERSITY; ORBION SPACE TECHNOLOGY, INC.

B64G1/1078F01D17/02F01D21/003F02K9/96G01M15/02G01M15/14

Abstract

Claims (21)

1. An interface assembly comprising:

a support member configured for direct coupling to and movement via a manipulation system;

a mounting member configured for direct coupling to an on-board propulsion system, wherein the interface assembly is configured to connect the on-board propulsion system to a testing facility; and

a plurality of channels, each channel of which extends from the mounting member to the support member, wherein at least one channel of the plurality of channels is configured to transmit fluid from the mounting member to the support member.

2. The interface assembly of claim 1 , wherein the plurality of channels extends at least partially within the mounting member.

3. The interface assembly of claim 1 , wherein the plurality of channels extends at least partially within the support member.

4. The interface assembly of claim 3 , wherein the plurality of channels extends at least partially within the mounting member.

5. The interface assembly of claim 1 , wherein the support member defines a longitudinal axis therethrough, and wherein the mounting member is spaced from the support member in the axial direction.

6. The interface assembly of claim 1 , further including a plurality of legs extending between and coupling the mounting member to the support member.

7. A method for testing an on-board propulsion system within a testing facility, the method comprising:

coupling the on-board propulsion system to a mounting member of an interface assembly, the interface assembly further including a support member connected to the mounting member, wherein at least one channel extends from the mounting member to the support member;

coupling the interface assembly to a manipulation system;

moving, via the manipulation system, the interface assembly coupled to the on-board propulsion system and to the manipulation system toward a chamber of the testing facility such that at least the mounting member is within the chamber;

connecting the moved interface assembly to the testing facility such that the interface assembly is configured to receive a fluid from the testing facility; and

operating the on-board propulsion system.

8. The method of claim 7 , wherein moving, via the manipulation system, the interface assembly toward a chamber of the testing facility such that at least the mounting member is within the chamber includes moving, via the manipulation system, the interface assembly entirely within the chamber of the testing facility.

9. The method of claim 7 , wherein moving, via the manipulation system, the interface assembly toward a chamber of the testing facility such that at least the mounting member is within the chamber includes moving, via the manipulation system, the interface assembly toward a chamber of the testing facility to engage a wall of the chamber.

10. The method of claim 7 , further including removing the atmosphere within the chamber to simulate an outer space environment.

11. The method of claim 7 , further including moving, via the manipulation system, the interface assembly away from the chamber of the testing facility such that the interface assembly is entirely outside of the chamber.

12. The method of claim 7 , wherein the steps herein are accomplished in fewer than 8 hours.

13. The method of claim 7 , further including de-coupling the interface assembly from the manipulation system.

Assignments (2)

Continuity (3)

References Cited (88)