Systems and methods for non-destructive testing of energetic materials
US9970920B2 · kind B2 · utility
0Cited by
10References
17Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Jun 4, 2015 |
| Grant date | May 15, 2018 |
| Priority date | — |
| Expiry date | Feb 4, 2036 |
Classification
- Technology area (CPC G)Physics
- CPC primaryG02B23/2476
- WIPO fieldMeasurement
- WIPO sectorInstruments
Abstract
A non-destructive testing system for propellant for a rocket is provided. The system includes an insertion tube having a first end and a second end in addition to a support sleeve configured to mate with a casing of the rocket. The insertion tube includes a channel that extends from the first end to the second end of the insertion tube to receive a probe and also includes a probe tip generally disposed at the second end of the channel. The support sleeve includes an insertion tube opening configured to receive the insertion tube and allow the insertion tube to slide along the support sleeve.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.