ADAMASat [Kentucky Space]
ADAMASat (Antenna Deployment and Mono-filament Actuator Satellite) was a sub-orbital payload designed and developed by Kentucky Space.
ADAMASat was built to the 2U CubeSat form factor and was battery powered. It tested during an about 8 minutes duration suborbital flight the KySat-1 antenna deployment mechanism and actuator circuit. The purpose was to gain confidence of the antenna deployment mechanism that consists of a mono-filament wire wrapped around the satellite to hold down it’s antennas, and a Nichrome cutter that burns the monofilament line to release the antennas. ADAMASat performed four tests of this mechanism while in space.
ADAMASat was flown on a suborbital 8 minutes flight on a Terrier Mk.70 Improved Malemute sounding rocket together with the Cal Poly 1U cubesat test on the SOCEM (SubOrbital CubeSat Experimental Mission) mission.
Nation: | USA |
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Type / Application: | Technology |
Operator: | Space Systems Lab |
Contractors: | Space Systems Lab |
Equipment: | |
Configuration: | CubeSat (2U) |
Propulsion: | None |
Power: | Batteries |
Lifetime: | < 1 hour |
Mass: | 2 kg |
Orbit: | suborbital |
Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
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ADAMASat | N/A | 27.03.2010 | WI LA-1-AML | * | Terrier Mk.70 Improved Malemute | with Cal Poly 1U, NASA 12.067GT |
* = suborbital