Interplanetary CubeSat Launch Opportunities and Payload Accommodations

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Interplanetary CubeSat Launch Opportunities and Payload Accommodations Roland Coelho, VP Launch Services Tyvak Nano-Satellite Systems Inc. +1(805) 704-9756 roland@tyvak.com Partnered with California Polytechnic State University (Cal Poly) San Luis Obispo, CA TERRAN ORBITAL

Tyvak CubeSat Launch Services Principals Have Extensive Launch Integration Experience Over a Decade Integrating CubeSats with Launch Vehicles First launch in 2003 Successfully Completed 18 Launch Campaigns 121 CubeSat integrated, 72 P-PODs 10 Different launch vehicles and 9 ranges worldwide 7+ Launch Campaigns Ongoing >40 CubeSats, >25 P-PODs NASA NPP with 3 P-PODs U.S. Govt with 8 P-PODs

Extensive POD Flight History 160 P-PODs Launched: 72 (25+ Manifested) CubeSats Launched In CP P-PODs: 121 (40+ Manifested) Today Number of CubeSats / Number of P- PODs 140 120 100 80 60 40 20 0 2003 2004 2005 2006 2007 2008 2009 2010 2011 2012 2013 2014 2015 2016

CubeSat Launch Services Launch Certifications Launch Coordination and Regulatory Approvals Experienced in ITAR International CubeSats on International LVs, International CubeSats on US LVs Radio Frequency Licenses IARU, FCC, NTIA, ITU Range Safety AFSPCMAN 91-710 Flexible Launch Manifesting CubeSat On-Orbit Operations Approvals From U.S./International Government Agencies Successfully managed and assisted CubeSats in obtaining: Export Control: Dept. of State, Commerce CubeSat Frequency Allocations: IARU, FCC, NTIA, ITU Orbital Debris Assessment Report (ODAR) and Re-Entry Analysis: NASA, AF, FCC Earth Imaging: NOAA

Available Environmental Processing and Testing Facilities Vibration Test Facilities 2 Vibration Tables Used for Qualification and Acceptance Testing of P-POD and CubeSat Hardware Random Vibration, Sine Vibe, and Sine Sweeps Thermal Vacuum Facilities Housed in a Portable Cleanroom Temp Range: -60 to 80C High Vacuum Data Acquisition System Used for Qualification, Acceptance, and Thermal Bake Out of Flight Hardware Clean Room Facilities Class 100,000 Nominal Capable of Class 10,000 and cleaner 28 x 8 ft. of Floor Space Locked Storage for Flight Hardware EMI/EMC Anechoic Chamber Facilities Tests for attenuation and CubeSat RF antenna patterns Supported CubeSat Testing at Other Facilities Commercial Test Facilities, NASA Ames, NASA WFF, NASA MSFC, SRI, NPS

Possible Capabilities for Interplanetary CubeSats Additional Capabilities for Sensitive CubeSats/Payloads Dependent on LV availability Planetary Protection Processing Nitrogen Purge Trickle Charging and Diagnostics Vibration Isolation Looking for feedback from community

Current Launch Opportunities Date Mission Destination Location Capacity 2015 U.S. Govt LEO Atlas V 24U 2015 U.S. Govt LEO Atlas V 24U Q1 2016 Commercial LEO Indian 12U Q1 2016 Commercial LEO Russian 12U Q1 2016 U.S. Govt Mars Atlas V 12U H1 2016 Commercial LEO Russian 9U H1 2016 Commercial LEO Indian 12U H2 2016 Commercial LEO/Escape Atlas V 24U+ H2 2016 Commercial LEO Indian 12U H2 2016 Commercial LEO Russian 24U+ H1 2017 Commercial GEO US 24U+

Current Launch Opportunities - GEO GEO Launch Opportunity Primary Spacecraft: SS/Loral Satellite Bus Maximum Mass: 60kg Maximum Volume: 1m x 0.5m x 0.4m CubeSat Form Factors: 1U to 27U+ Launch: Early Q1 2017 Delivery for Integration: ~Sept. 2016 Cost: ~$100,000 USD per kg (negotiable) Contract Signing: June/July 2015

Current Launch Opportunities - Interplanetary 1 st Commercial Interplanetary Launch Opportunity! Very Quick Turnaround Needed Launch Details Launch Vehicle: ULA Atlas V CubeSat Form Factors: 1U to 12U Capacity Available: 108U Launch: Q3 2016 Delivery for Integration: June/July 2016 Cost: ~$700,000 USD per 3U to Elliptical or Escape Orbit Contract Signing: ASAP Orbit Option #1 LEO SSO 620km Orbit Option #2 Highly Elliptical Perigee: ~620km Apogee: Between Lunar and 1,000,000km Phasing possible for lunar flyby 10-40 day orbit period ~40 m/s at perigee to go escape Orbit Option #3 Earth Escape Orbit C3 of ~0.1

Conclusions Looking for feedback from Interplanetary CubeSat community on additional requirements and needs Current interplanetary launch opportunity in Q3 2016, need to act fast if interest/funding is available Collaboration with science teams creates new opportunities Roland Coelho, VP Launch Services Tyvak Nano-Satellite Systems Inc. +1(805) 704-9756 roland@tyvak.com