Publication Date:
2013-08-31
Description:
A new deployable and retractable telescoping boom capable of high deployed stiffness and strength is described. Deployment and retraction functions are controlled by simple, reliable, and fail-safe latches between the tubular segments. The latch and a BI-STEM (Storable Tubular Extendible Member) actuator work together to eliminate the need for the segments to overlap when deployed. This yields an unusually lightweight boom and compact launch configuration. An aluminum space-flight prototype with three joints displays zero structural deadband, low hysteresis, and high damping. The development approach and difficulties are discussed. Test results provide a joint model for sizing flight booms of any diameter and length.
Keywords:
MECHANICAL ENGINEERING
Type:
NASA. Lewis Research Center, The 28th Aerospace Mechanisms Symposium; p 323-338; NASA-CP-3260
Format:
application/pdf
Permalink
