Technologies The NASA Space Telerobotics Program

Space Modular Manipulators

The unique thermal, vacuum and gravitational conditions of space drive the robot design process towards solutions that are much different from the typical laboratory robot. JSC's A&R Division is at the forefront of this design effort with the prototypes being built for the Space Modular Manipulators (SMM) project. The first SMM joint prototype has completed its thermal-mechanical-electrical design phase, is now under construction in the JSC shops, and is scheduled for thermal-vac chamber tests in FY94.

FY93 was the SMM project's first year, initiating the effort with a MITRE Corporation review of the existing space manipulator design efforts (RMS and FTS) and interaction with ongoing development teams (RANGER, JEM, SPDM, STAR and SAT). Below this system level, custom component vendors for motors, amplifiers, sensors and cables were investigated to capture the state-of-the-art in space robot design. Four main design drivers were identified as critical to the development process:

  1. Extreme Thermal Conditions;
  2. High Reliability Requirements;
  3. Dynamic Performance; and
  4. Modular Design.
While these design issues are strongly coupled, most robot design teams have handled them independently, resulting in an iterative process as each solution impacts the other problems. The SMM design team has sought a system level approach that will be demonstrated as prototypes which will be tested in the JSC thermal-vacuum facilities.

The thermal-vacuum conditions of space are the most dramatic difference between typical laboratory robot and space manipulator design requirements. Manufacturing robots operate in climate controlled, \|O(+,-)2K factory environments, where space manipulators must be designed for \|O(+,-)75K temperature variations with 1500 W/m2 of solar flux. Despite these environmental extremes, the technology to model and control robot precision over a wide temperature range can be applied to terrestrial robotic operations where the extreme precision requirements demand total thermal control, such as in semiconductor manufacturing and medical robot applications.

Thermal conditions impact reliability by cycling materials and components, adding to the dynamic loading that causes typical robot fatigue and inaccuracy. MITRE built a customized thermal analysis model, a failure analysis model using FEAT, and applied the fault tolerance research funded by JSC at the University of Texas. The strategy is to layer low level redundancy in the joint modules with a high level, redundant kinematic system design, where minor joint failures can be masked and serious failures result in reconfigured arm operation. In this approach, all four design drivers were addressed in the selection of the appropriate level of modular design as a 2-DOF joint module.

The major technical accomplishments for the FY93 SMM project are:

  1. Conceptual and detailed design of first joint prototype;
  2. Detailed design and fabrication of thermal-vacuum test facility;
  3. Custom design of thermal-vac rated motors, bearings, sensors and cables; and
  4. Published two technical papers (R. Ambrose & R. Berka) on robot thermal design.

Point of Contact:
John T. Chladek
Mail Stop EF-23
Johnson Space Center
Houston, TX 77058
713-483-1528
jchladek@jsc.nasa.gov



Program Description Major Projects Program Plans Participants & Facilities Technologies
Photo Log Robot Tools Cool Robot of the Week Internet Robotics Resources Real Robots on the Web

Telerobotics Program page

Please email the site webmaster with any comments, criticisms or corrections for this page.
Maintained by: Dave Lavery
Last updated: May 10, 1996