Mr. Jason Gordon Profile

Jason Gordon

at Boeing Co

SPIE Involvement:

Author

Publications (1)

This will count as one of your downloads.

You will have access to both the presentation and article (if available).

DOWNLOAD NOW

This content is available for download via your institution's subscription. To access this item, please sign in to your personal account.

Email or Username Forgot your username?

Password Forgot your password?

Show

Keep me signed in

No SPIE account? Create an account

Proceedings Article | 5 May 2005 Paper

Structural sensor testing for space vehicle applications

Jerry Huang, John Rose, Jason Gordon, Robert Boucher

Proceedings Volume 5762, (2005) https://doi.org/10.1117/12.607302

KEYWORDS: Sensors, Structural health monitoring, Nondestructive evaluation, Fiber optics sensors, Composites, Finite element methods, Fiber optics, Fiber optics tests, Decision support systems, Ultrasonics

Read Abstract +

The Boeing Company is funded by Air Force Research Laboratory (AFRL) to perform research and development activities on Structural Health Monitoring (SHM) and Assessment Techniques for Advanced Aerospace Vehicles. This effort includes two SHM aspects, i.e., on-board sensors and ground based NDE techniques. The first aspect focuses on prototyping a SHM system that integrates several different types of sensors to generate structural health information based on real-time or near real-time sensor data. The second aspect focuses on a ground system that provides a linkage between the on-board sensors and ground based NDE techniques with a prototype system capable of rapidly gathering and interpreting structural health information. They can be viewed as two parts of a SHM system that are complimentary to one another. Developing such an SHM system is intended to help advance aerospace vehicle's safety and reliability, satisfy the required turnaround time, reduce cost and cycle time in design, operation and maintenance. The primary vehicle platform considered for this program is the Space Operation Vehicle (SOV)¹, a future high speed vehicle. The baseline vehicle description will be used to determine system requirements for a SHM/NDE system and to evaluate candidate technologies throughout the technology down select process. This paper will discuss an evaluation test in which candidate sensors and NDE methods are applied to space structure components tested at a simulated flight load environment.

My Library

You currently do not have any folders to save your paper to! Create a new folder below.

Folder Name

Folder Description

View contact details

UPDATE YOUR PROFILE

Is this your profile? Update it now.

Sign into your SPIE.org account

Don’t have a profile and want one?

Create an account on SPIE.org

Access to the requested content is limited to institutions that have purchased or subscribe to SPIE eBooks. You are receiving this notice because your organization may not have SPIE eBooks access.*

*Shibboleth/Open Athens users─please sign in to access your institution's subscriptions.

To obtain this item, you may purchase the complete book in print or electronic format on SPIE.org.

ORGANIZATIONAL
Sign in with credentials provided by your organization.

Organizational Username

Organizational Password

Show/Hide Password

INSTITUTIONAL
Select your institution to access the SPIE Digital Library.

SELECT YOUR INSTITUTION

PERSONAL
Sign in with your SPIE account to access your personal subscriptions or to use specific features such as save to my library, sign up for alerts, save searches, etc.

PERSONAL SIGN IN

No SPIE Account? Create one

PURCHASE THIS CONTENT

SUBSCRIBE TO DIGITAL LIBRARY

50 downloads per 1-year subscription

Members: $195

Non-members: $335 ADD TO CART

25 downloads per 1 - year subscription

Members: $145

Non-members: $250 ADD TO CART

PURCHASE SINGLE ARTICLE

Includes PDF, HTML & Video, when available

Members:

Non-members: ADD TO CART

Keywords/Phrases

Search In:

Publication Years