d) = 11,000 km, = 10 m2/kg e) = 14,864 km, = 10 m2/kg f) = 18,000 km, = 10 m2/kg a A/m a A/m a A/m g) = 11,000 km, = 20 m2/kg h) = 14,864 km, = 20 m2/kg i) = 18,000 km, = 20 m2/kg a A/m a A/m a A/m Fig. 2: Eccentricity-ϕ phase space evolution for the planar simplified case of The bold lines represent the J2+SRP. separatrices in correspondence of the saddle point and zero eccentricity Hamiltonian, the shaded area marks orbit heights lower than one Earth radius. Semi-major axis of 11,000 km (first column), 14,864 km (second column) and 18,000 km (third column). Area-to-mass of 5 m2/kg (first row), 10 m2/kg (second row) and 20 m2/kg (third row).
d) a = 11,000 km, A/m = 10 m2/kg e) a = 14,864 km, A/m = 10 m2/kg f) a = 18,000 km, A/m = 10 m2/kg g) a = 11,000 km, A/m = 20 m2/kg h) a = 14,864 km, A/m = 20 m2/kg i) a = 18,000 km, A/m = 20 m2/kg Fig. 2: Eccentricity-ϕ phase space evolution for the planar simplified case of J2+SRP. The bold lines represent the separatrices in correspondence of the saddle point and zero eccentricity Hamiltonian, the shaded area marks orbit heights lower than one Earth radius. Semi-major axis of 11,000 km (first column), 14,864 km (second column) and 18,000 km (third column). Area-to-mass of 5 m2/kg (first row), 10 m2/kg (second row) and 20 m2/kg (third row).
Colombo_C_Lucking_C_McInnes_CR_Pure_Orbital_dynamics_of_high_area_to_mass_ratio_spacecraft_with_J2_and_solar_radiation_pressure..._communications_services_Dec_2012.docx