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200g Balloon Launch Parameters

Scott Breitengross Mar 27, 2008 Trajectory group, Delta V, Saturn V, Feasability Determination, 1 kg Final Design Final Presentation. 200g Balloon Launch Parameters. Tables generated from trajectory code output data. Trajectory. Δ V Equations.

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200g Balloon Launch Parameters

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  1. Scott BreitengrossMar 27, 2008Trajectory group, Delta V, Saturn V, Feasability Determination, 1 kg Final Design Final Presentation AAE 450 Spring 2008

  2. 200g Balloon Launch Parameters Tables generated from trajectory code output data AAE 450 Spring 2008 Trajectory

  3. ΔV Equations • Where μ is the gravitational constant and Rp is the Radius of the periapsis from the center of the earth • Where D(t) is the drag profile and m(t) is the mass profile • Where g(t) is the gravity profile and γ(t) is the flight path angle • Where Reis the radius of the Earth, φ is the launch latitude, and td is time in a day in seconds *all equations generated in Space Propulsion, Analysis and Design Book.

  4. 200g Additional Data Orbit and model generated by trajectory code

  5. Where T(t) is the Thrust profile and m(t) is the mass profile References: Humble, Ronald W., Henry, Gary N., Larson, Wiley J., Space Propulsion Analysis and Design. The McGraw-Hill Companies Inc. St. Louis, Missouri, 1995.

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