Piezo-Electric Actuators on Nano-satellite Unit Testbed
(PEANUT)

About PEANUT
The objective of the Piezo Electric Actuators on Nanosatellite Unit Testbed (PEANUT) Experiment is the development and testing of novel, piezo-electric actuators on satellite platforms. It aims to show the feasibility of this actuator type, demonstrate their functionality and verify whether these actuators can reduce vibrations compared to regular ones. PEANUT consists of two separate units, the Rocket Mounted Unit (RMU) and the Free Fall Unit. The RMU will eject the FFU from the rocket to test the actuator‘s performance in free fall. In the FFU piezo-electric actuators, an accelerometer to evaluate the actuator‘s performance and an Attitude Determination System are contained. During free fall the goal is to perform detumbling and subsequent three-axis control of the FFU by using the piezoelectric actuators and verifying their vibrational performance. Flight and mission data are fully saved and recovered by means of a parachute and communications system.
Experiment Concept
The experiment will get launched aboard the REXUS launch vehicle and ejected after motor burn-out and despin of the rocket. During the free fall phase we will test the piezo-electric actuators. At about 4 km altitude the Free Fall Unit (FFU) deploys parachutes to safely touch-down to ground to recover the experiment and data gathered during the flight.

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