This report evaluates adhesive bonding techniques used to mount an optic intended for spaceflight application. Based on launch and operational environments, finite elements analysis and information gathered from previous programs, three variables were identified. Eight test samples were designed, fabricated and then tested for the effect that extreme temperatures have on the adhesive joint between the optic and mount. Results revealed that the adhesive's tensile strength was not affected by thermal stresses; however, stability results were inconclusive.

• This report represents the work of one or more WPI undergraduate students submitted to the faculty as evidence of completion of a degree requirement. WPI routinely publishes these reports on its website without editorial or peer review.

Creator

• Ziemba, Rebeccah J.
• Culver, Wesley Paul
• Rockwell, Justin A.

Publisher

• Worcester Polytechnic Institute

Identifier

• 06D008M

Advisor

• Tryggvason, Gretar

Year

• 2006

Center

• MIT Lincoln Laboratory-Lexington, Massachusetts Project Center - MQP

Sponsor

• MIT Lincoln Laboratory

Date created

• 2006-01-01

Resource type

• Major Qualifying Project

Major

• Mechanical Engineering

Rights statement

• In Copyright