IP Library › Granted Patent US 8,525,705
Granted Patent B1
US 8,525,705 · App. 12/802,449 · Granted Sep 3, 2013

Apparatus and method for detecting defects in solid rocket motor propellant

Inventor: Craig Michael Lopatin (Washington, DC)
Assignee: The United States of America as Represented by the Secretary of the Navy
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 8,525,705
App. No.
12/802,449
Granted
Sep 3, 2013
Kind
B1
Abstract

A solid rocket motor having a liner surrounding a propellant includes an array of transmitter elements and receiver elements disposed within the liner. Transmitter electronics provide the transmitter elements with a transmit signal and receiver electronics receive the outputs of the receiver elements. The outputs are analyzed to determine any defects in the propellant.

Claims (15)

1. An apparatus for detecting defects in a propellant contained within a casing, comprising:

a liner being disposed between said propellant and said casing;

an array of RF transmitter elements and RF receiver elements being disposed within said liner and surrounding said propellant,

wherein said propellant is a solid rocket motor propellant; and

a flexible sheet surrounding said propellant,

wherein said RF transmitter elements and said RF receiver elements are disposed on said flexible sheet, and

wherein said RF receiver elements are alternately arranged with said RF transmitter elements around said propellant.

2. The apparatus of claim 1 , further comprising transmitter electronics for providing said RF transmitter elements with a transmit signal; and receiver electronics for receiving output signals from said RF receiver elements.

3. The apparatus of claim 2 , wherein said transmitter electronics and said receiver electronics are contained within said casing, and

wherein said casing is a rocket casing.

4. The apparatus of claim 1 , wherein said liner comprises an elastomeric material.

5. The apparatus of claim 2 , further comprising a microprocessor for processing said output signals for providing an indication of defects within said propellant.

6. The apparatus of claim 1 , wherein said RF transmitter elements and said RF receiver elements are adhesively attached to said flexible sheet.

7. The apparatus of claim 1 , wherein said RF transmitter elements and said RF receiver elements are deposited on said flexible sheet by chemical vapor deposition.

8. The apparatus of claim 1 , wherein said flexible sheet is disposed in said liner.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 29, 2010
From: LOPATIN, CRAIG M.
To: NAVY, THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE
Reel/Frame 024622/0181 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 28, 2010
From: LOPATIN, CRAIG M.
To: NAVY, UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE, THE
Reel/Frame 024606/0021 →