Please make a donation to support Gunter's Space Page.
Thank you very much for visiting Gunter's Space Page. I hope that this site is useful and informative for you.
If you appreciate the information provided on this site, please consider supporting my work by making a simple and secure donation via PayPal. Please help to run the website and keep everything free of charge. Thank you very much.

MEMS Picosat (DARPA Picosat)

MEMS 1A & MEMS 1B [The Aerospace Corp.]

The mission will usher in a spaceflight program to validate MEMS - tiny microelectromechanical systems being developed under sponsorship of DARPA, the Defense Advanced Research Projects Agency.

The experiment calls for two tethered picosatellites, each weighing less than one-half-pound and not much larger than a deck of cards, to be released into low Earth orbit by the OPAL satellite. OPAL is the Orbiting Picosat Automated Launcher built by Stanford University students at the school's Space Systems Development Laboratory.

The primary goal of the DARPA/Aerospace picosasts on this mission is to validate microelectromechanical systems (MEMS) radio frequency switches designed by Rockwell Science Center, Thousand Oaks, Calif. Other MEMS devices are to be validated on subsequent picosat missions. The mission also is designed to demonstrate the principles of how constellations of nanosatellites, slightly larger than picosats, will operate in the future.

The two orbiting picosats are to be tethered because they will communicate via micropower radios. The tether will keep them within range of each other for crosslink purposes. In addition, the tether contains thin strands of gold wire to facilitate radar tracking by U.S. Space Command. Concepts for the future involve optical communication via fiberoptic tethers and other cluster architectures for miniature satellites for which experience with tethers is useful.

Another DARPA/Aerospace picosat mission involving a Minotaur booster and an Air Force Research Laboratory MightySat 2.1 satellite was conducted in July 2000. Plans call for the picosats to be released on command from MightySat 2.1 after spending specified time on orbit. A more complex mission followed in 2003.

Nation: USA
Type / Application: Experimental
Operator: DARPA
Contractors: Aerospace Corp.
Equipment: Tether
Configuration: Box
Propulsion: None
Power: Batteries
Lifetime:
Mass: 0.4 kg
Orbit: 750 km × 800 km, 100.22
Satellite COSPAR Date LS Launch Vehicle Remarks
MEMS 1A (Pico 21) 2000-004H 27.01.2000 Va CLF Minotaur-1 with JAWSAT, FalconSat1, ASUSat 1, OCSE, OPAL, MEMS 1B, STENSAT, JAK, Thelma, Louise
MEMS 1B (Pico 23) 2000-004H 27.01.2000 Va CLF Minotaur-1 with JAWSAT, FalconSat 1, ASUSat 1, OCSE, OPAL, MEMS 1A, STENSAT, JAK, Thelma, Louise
MEMS 2A (Pico 20) 2000-042C 19.07.2000 Va CLF Minotaur-1 with MightySat 2.1
MEMS 2B (Pico 22) 2000-042C 19.07.2000 Va CLF Minotaur-1 with MightySat 2.1

References: