SOUTH ATLANTIC ANOMALY AND CUBESAT DESIGN CONSIDERATIONS
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1 SOUTH ATLANTIC ANOMALY AND CUBESAT DESIGN CONSIDERATIONS 09 AUG 2015 Integrity Service Excellence Presenter Judy A. Fennelly, DR-III, RVB Air Force Research Laboratory Space Vehicles Directorate 1
2 South Atlantic Anomaly and CubeSat Design Considerations Judy A. Fennelly a, William R. Johnston a, Daniel M. Ober a, Gordon R. Wilson a, T. Paul O Brien b and Stuart L. Huston c a Air Force Research Laboratory, Space Vehicles Directorate, 3350 Aberdeen Avenue, Kirtland AFB, NM 87117, b Aerospace Corporation, Conference Center Drive, Chantilly, VA c Atmospheric and Environmental Research, Inc., 131 Hartwell Avenue, Lexington, MA SPIE Paper
3 South Atlantic Anomaly (SAA) & CubeSat Design Considerations 1.0 SAA Space Environment 2.0 Space Effects in the SAA 3.0 SAA Mitigation Strategies 3
4 AE9/AP9/SPM Radiation Model Design and Mission Planning Using a new combined set of models for the space environment determination needed for CubeSat design and mission planning Expanded energy coverage: kev plasma to GeV protons Spatial coverage for all orbit regimes, including tailored coverage for high resolution in LEO Model AE9 AP9 SPM Species e - H + e -, H +, He +, O + Energies 40 kev 10 MeV Range in L 0.98 < L * < kev 2 GeV (V1.20) 0.98 < L * < kev (e - ); kev (H +, He +, O + ) 2 < L m < 10 GPS, 95% Confidence, Worst Case 24-hour average 10 7 Flux #/cm 2 /s/mev years 1 years 2 years years 4 years years 6 years 7 years years 9 years 10 years Energy, MeV 4
5 What Type of Run Spec Type Type of Run Duration Notes Total Dose Perturbed Mean Several orbits or days SPME+AE9, SPMH+AP9+Solar Displacement Damage (proton fluence) Perturbed Mean Several orbits or days AP9+Solar Proton SEE (proton worst case) Internal Charging (electron worst case) Monte Carlo Full Mission AP9+Solar Monte Carlo Full Mission AE9 (no SPME) Run 40 scenarios through either static Perturbed Mean or dynamic Monte Carlo Compute statistics by comparing results across scenarios (e.g., in what fraction of scenarios does the design succeed) Do not include plasma (SPM*) models in worst case runs 5
6 Data Sets Temporal Coverage plasma electrons protons AP8 released AE8 released new in V1.20 6
7 SAA Proton Flux Source: Horn of the Inner Radiation Belt 7
8 SAA Couples Horn With a Weak Surface Magnetic Field 8
9 AP9 V1.20 Validation SAA >35 MeV protons SAA flux profiles are improved in V1.20 as compared to POES observations Ratio of AP9 V1.20 median to POES data East-west profile North-south profile electron contamination POES MEPED background 9
10 SAA Spatial Extent: AE9/AP9/SPM Radiation Model 10
11 SAA Spatial Extent (300Km): AE9/AP9/SPM Radiation Model 11
12 Use Directional or Omnidirectional Fluxes? DMSP-F Average Background Counts Directional Flux for Fixed Orientation with respect to Earth Omnidirectional Flux for Random Orientation 12
13 SAA Drift Rate Over Time From DMSP SSJ contamination Satellite Year Latitude Longitude F F F F F F F F F F From AP9 V1.20 mean >30 MeV Year Latitude Longitude location of SAA peak, location of SAA peak, AP9 >400 MeV DMSP SSJ DMSP SSJ AP9 >30 MeV AP9 >16 MeV 13
14 AE9/AP9 Website We have launched a dedicated web site for the AE9/AP9 project hosted by AFRL s Virtual Distributed Laboratory: The latest version of the model may be downloaded from this site after creating an account Summaries and model documentation are also available (no account needed) Future news and releases will be announced through the website 14
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