Title :
Mechanical Description of the Mars Climate Sounder Instrument
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA
Abstract :
This paper introduces the Mars Climate Sounder (MCS) Instrument of the Mars Reconnaissance Orbiter (MRO) spacecraft. The instrument scans the Martian atmosphere almost continuously to systematically acquire weather and climate observations over time. Its primary components are an optical bench that houses dual telescopes with a total of nine channels for visible and infrared sensing, and a two axis gimbal that provides pointing capabilities. Both rotating joints consist of an integrated actuator with a hybrid planetary/harmonic transmission and a twist cap section that enables the electrical wiring to pass through the rotating joint. Micro stepping is used to reduce spacecraft disturbance torques to acceptable levels while driving the stepper motors. To ensure survivability over its four year life span, suitable mechanical components, lubrication, and an active temperature control system were incorporated. Some life test results and lessons learned are provided to serve as design guidelines for actuator parts and flex cables.
Keywords :
Mars; aerospace control; aerospace instrumentation; planetary atmospheres; planetary remote sensing; space vehicles; stepping motors; temperature control; torque; Mars Climate Sounder instrument; Mars Reconnaissance Orbiter spacecraft; Martian atmosphere; active temperature control system; climate observations; dual telescopes; mechanical components; micro stepping; spacecraft disturbance torques; stepper motors; weather observations; Actuators; Atmosphere; Instruments; Mars; Optical devices; Optical sensors; Reconnaissance; Space vehicles; Telescopes; Wiring;
Conference_Titel :
Aerospace Conference, 2008 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4244-1487-1
Electronic_ISBN :
1095-323X
DOI :
10.1109/AERO.2008.4526543