Final answer:
The angular momentum of the satellite about its center is 497,785.6 kg⋅m^2/s.
Step-by-step explanation:
To calculate the angular momentum of the satellite about its center, we need to consider the angular momentum of the main body and the antennas separately.
The angular momentum of the main body can be calculated using the formula: L = I × ω, where I is the moment of inertia and ω is the angular velocity. For a solid sphere, the moment of inertia is given by I = (2/5) × m × r^2, where m is the mass and r is the radius. Plugging in the values, we get I = (2/5) × 10000 kg × (2.0 m)^2 = 80000 kg⋅m^2. The angular momentum of the main body is then L_main = 80000 kg⋅m^2 × 6.2 rev/s = 496000 kg⋅m^2/s.
Each antenna can be considered as a rod rotating around one end, so the moment of inertia is given by I = (1/3) * m * L^2, where L is the length. Plugging in the values, we get I = (1/3) × 16 kg × (3.0 m)^2 = 144 kg⋅m^2. The angular momentum of each antenna is then L_antenna = 144 kg⋅m^2 × 6.2 rev/s = 892.8 kg⋅m^2/s.
The total angular momentum of the satellite is the sum of the angular momenta of the main body and the antennas: L_total = L_main + 2 × L_antenna = 496000 kg⋅m^2/s + 2 × 892.8 kg⋅m^2/s = 496000 kg⋅m^2/s + 1785.6 kg⋅m^2/s = 497785.6 kg⋅m^2/s.