"The De-orbit Plan" as submitted in the approved license extension.
Although not subject to the requirements of Section 25.283(a) of the Commission’s rules, at the end of the operational life of the satellite, DIRECTV will maneuver DIRECTV-4S into a disposal orbit with an altitude no less than that calculated using the IADC formula: 36,021 km + (1000·CR·A/m). The calculated value of CRA/m in this instance is based on the following parameters: CR = Solar Pressure Radiation Coefficient = 1.2 A = Total Solar Pressure Area = 90 m 2 m = Dry Mass of Satellite = 2132.5 kg Using these values in the IADC formula results in a minimum de-orbit altitude of 36,072 km, or approximately 286 km above geosynchronous altitude. To provide adequate margin, the nominal disposal orbit will be increased above this calculated value of 36,072 km to a value of 36,086 km, resulting in a disposal orbit approximately 300 km above geosynchronous altitude. Approximately 16.4 kg of propellant will be allocated and reserved for final orbit raising maneuvers to this altitude. This value was determined through a detailed propellant budget analysis. In addition, DIRECTV has assessed fuel gauging uncertainty and this budgeted propellant provides an adequate margin of fuel reserve to ensure that the disposal orbit will be achieved despite such uncertainty.