Problem 2.36 A hyperbolic earth departure trajectory has a perigee altitude of 250 km and a perigee speed of 11 km/s. (a) Calculate the hyperbolic excess speed (km/s). (b) Find the radius (km) when the true anomaly is 100 degrees. (c) Find v, and v₁ (km/s) when the true anomaly is 100 degrees.

Classical Dynamics of Particles and Systems
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ISBN:9780534408961
Author:Stephen T. Thornton, Jerry B. Marion
Publisher:Stephen T. Thornton, Jerry B. Marion
Chapter10: Motion In A Noninertial Reference Frame
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Problem 2.36 A hyperbolic earth departure trajectory has a perigee altitude of 250 km and a perigee
speed of 11 km/s.
(a) Calculate the hyperbolic excess speed (km/s).
(b) Find the radius (km) when the true anomaly is 100 degrees.
(c) Find v, and v₁ (km/s) when the true anomaly is 100 degrees.
Transcribed Image Text:Problem 2.36 A hyperbolic earth departure trajectory has a perigee altitude of 250 km and a perigee speed of 11 km/s. (a) Calculate the hyperbolic excess speed (km/s). (b) Find the radius (km) when the true anomaly is 100 degrees. (c) Find v, and v₁ (km/s) when the true anomaly is 100 degrees.
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