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Launch&Orbit / Mogens Blanke Satellite Systems and Design DTU 20-31 August 2001 Launch and Orbits Mogens Blanke Automation

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Presentation on theme: "Launch&Orbit / Mogens Blanke Satellite Systems and Design DTU 20-31 August 2001 Launch and Orbits Mogens Blanke Automation"— Presentation transcript:

1 Launch&Orbit / Mogens Blanke Satellite Systems and Design DTU August 2001 Launch and Orbits Mogens Blanke Automation

2 Launch&Orbit / Mogens Blanke Sequence of events 11:39:52 Delta II raketten affyres. 11:40:25 Lydmuren gennembrydes. 11:40:38 Maksimum motorkraft 11:43:16 Hovedmotoren stoppes. 11:43:24 1. trin og 2. trin separeres. 11:43:29 2. trin startes. 11:50:51 2. trin stoppes. 12:31:14 2. trin genstartes 1. gang.

3 Launch&Orbit / Mogens Blanke

4 Kepler’s laws Kepler provided three laws for planetary motion, based on Brahe’s observations. 1. The orbit of a planet is an ellipse with the Sun located at one focus 2. The radius vector drawn from the Sun to a planet sweeps out equal areas in equal time 3. Planetary periods of revolution are proportional to mean distance to the Sun ^3/2

5 Launch&Orbit / Mogens Blanke Newton’s results The laws of NewtonPhysical parameters

6 Launch&Orbit / Mogens Blanke Two-body problem

7 Launch&Orbit / Mogens Blanke

8 Orbit radius and velocity

9 Launch&Orbit / Mogens Blanke Potential and kinetic energy Energy Parameters


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