AMSAT-NA FOX Satellite Program
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1 AMSAT-NA FOX Satellite Program Review, Status, and Future JERRY BUXTON, NØJY, AUTHOR AMSAT VP-ENGINEERING
2 Review FOX-1 - WHY IT IS, WHAT IT IS
3 Fox Development Strategy Take advantage of large and growing interest in CubeSats Develop family of CubeSats with ham radio transponders that are attractive for hosting science experiments Partner with universities to develop joint science and education missions Get a free launch via the NASA ELaNa program
4 Fox-1: AMSAT-NA s First CubeSat Smallest satellite previously built by AMSAT-NA was a 25 cm (approximately 10 inch) cube Fox-1 is10 cm (approximately 4 inches) per side Miniaturization not attempted before by AMSAT-NA Coaxing maximum power from limited solar panel area Insure stability and robustness of the avionics bus in the environment of space Success gives us CubeSat design heritage and puts AMSAT-NA back in space
5 Fox -1 CubeSat Size: 1U Mass: 1.33 kg RF Power: 800 mw max Mission Description: To inspire, engage and educate the next generation Two-way FM communications transponder MEMS Gyro Experiment (Penn State) Low Energy Proton Experiment (Vanderbilt) JPEG Camera (Virginia Tech)
6 University Experiment Payloads on Fox-1 Virginia Tech EXP4 Filler/Lens Hole VT Camera Vanderbilt EXP1 Vanderbilt Sensors Vanderbilt Controller Penn State - Erie MEMS Gyros (on IHU board)
7 Fox-1 Block Diagram and Avionics System Bus 6 Solar Panels Power Supply Battery 70 cm Science Payloads IHU Power bus Magnetic Attitude Control 2 m Telemetry RF Rx RF Tx
8 Fox-1 Block Diagram and Avionics System Bus 6 Solar Panels Power Supply Battery 70 cm Science Payloads IHU Power bus Magnetic Attitude Control 2 m Telemetry RF Rx RF Tx
9 Fox-1 Block Diagram and Avionics System Bus 6 Solar Panels Power Supply Battery 70 cm Science Payloads IHU Power bus Magnetic Attitude Control 2 m Telemetry RF Rx RF Tx
10 Fox-1 Block Diagram and Avionics System Bus 6 Solar Panels Power Supply Battery 70 cm Science Payloads IHU Power bus Magnetic Attitude Control 2 m Telemetry RF Rx RF Tx
11 Fox-1 Block Diagram and Avionics System Bus 6 Solar Panels Power Supply Battery 70 cm Science Payloads IHU Power bus Magnetic Attitude Control 2 m Telemetry RF Rx RF Tx
12 Fox-1 Block Diagram and Avionics System Bus 6 Solar Panels Power Supply Battery 70 cm Science Payloads IHU Power bus Magnetic Attitude Control 2 m Telemetry RF Rx RF Tx
13 RF Transmitter System Engineering Model
14 RF Transmitter System Shield
15 Fox-1 Block Diagram and Avionics System Bus 6 Solar Panels Power Supply Battery 70 cm Science Payloads IHU Power bus Magnetic Attitude Control 2 m Telemetry RF Rx RF Tx
16 Fox-1 Block Diagram and Avionics System Bus 6 Solar Panels Power Supply Battery 70 cm Science Payloads IHU Power bus Magnetic Attitude Control 2 m Telemetry RF Rx RF Tx
17 Power Supply System Engineering Model
18 Fox-1 Block Diagram and Avionics System Bus 6 Solar Panels Power Supply Battery 70 cm Science Payloads IHU Power bus Magnetic Attitude Control 2 m Telemetry RF Rx RF Tx
19 Battery System Engineering Model w/o batteries
20 Fox-1 Block Diagram and Avionics System Bus 6 Solar Panels Power Supply Battery 70 cm Science Payloads IHU Power bus Magnetic Attitude Control 2 m Telemetry RF Rx RF Tx
21 Fox-1 Block Diagram and Avionics System Bus 6 Solar Panels Power Supply Battery 70 cm Science Payloads IHU Power bus Magnetic Attitude Control 2 m Telemetry RF Rx RF Tx
22 Status FOX-1 WHERE WE ARE, WHAT IS NEXT
23 Two Launch Opportunities! May on ELaNa XI possible if there s a vacancy AFSPC ULTRASat mission Planned orbit is 389 km x degrees inclination Expected orbit lifetime is 6.5 years August 2015 on ELaNa XII MOST LIKELY NRO GRACE mission our original manifest Planned orbit is 470 km x degrees inclination Expected orbit lifetime is 11 years
24 Our Ride (example)
25 Our Ride (example) FOX-1
26 Our Ride (example)
27 Fox-1 Status Milestones May Engineering Unit Integration and Testing June Critical Design Review August Flight Model and Flight Spare complete Day In The Life testing September Vibration Testing and Thermal Vacuum (bakeout) complete September Mission Readiness Review October Completion and Hands Off Fox-1 sits on the shelf waiting for delivery in January 2015
28 Fox-1 Status Fox-1B RadFXSat (CSLI 4 Feb 2013) Use Flight Spare hardware from Fox-1 Flight Spare experiments from Fox-1 returned to partners Vanderbilt RadFXSat experiment installed Operates simultaneously with Transponder Reset and start again CDR, Flight Model and Flight Spare integration and testing, Launch provider required testing, Deliver to launch provider Ready in Second Half 2015
29 Fox-1 Status Fox-1C and Fox-1D On the shelf and ready to fly, requiring only solar cells (Of course, all of the other integration and testing is still required!) Looking for university partners You provide the experiments, we provide the communications for your data Partner for launch opportunities Amateur radio transponder during or after experiment phase EXP4 EXP3 EXP2 EXP1
30 Fox-1C gets a launch! AMSAT teamed with Spaceflight. Inc for integration and launch on SHERPA to sun-synchronous in Q Fundraising campaign to raise $125,000 for expenses over next 12 months Experiment proposals under investigation Donate via amsat.org, or via Martha at AMSAT office Please consider a recurring donation (Paypal or President s Club)
31 Future FOX-2 AND BEYOND
32 Fox-2 Flight heritage and track record from Fox-1 series 3U CubeSat Software Defined Transponder Higher power, more modes/bands Attitude Determination and Control Development underway
33 And Beyond CubeSat market has not yet reached a plateau Larger sizes are becoming more common 3U, 6U, even 12U Exploration and research leading to expanded possibilities Propulsion - higher orbits (but not allowed on ELaNa) Satellites in formation Several possibilities and partnerships being explored We are ALWAYS exploring new opportunities!
34 Any Questions?
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