TiPS in-orbit configuration

Technical Features

• Jettisoned from host vehicle after primary mission completion
• Fully deployed payload of two separate bodies connected by 4 km (2.5 mile) tether
• Norton mounted closest to host vehicle has no electronics
• Ralph contains electronics, tether deployer, and instrumentation

Objectives

• Enhanced understanding of "libration," the pendulum-like motion of endmasses about system center of mass
• Collect data on tether's susceptibility to damage by space debris
• Successfully deployed by satellite in 1996, still operational 1999

TiPS pre-deployment configuration