orbitalmechanics
Differences
This shows you the differences between two versions of the page.
| Previous revision | |||
| — | orbitalmechanics [2024/01/31 04:08] (current) – external edit 127.0.0.1 | ||
|---|---|---|---|
| Line 1: | Line 1: | ||
| + | 1 Newton = 1 kg * m/s^2 | ||
| + | |||
| + | == Vehicle | ||
| + | |||
| + | 80kg (175 lbs) | ||
| + | |||
| + | 80kg in earth' | ||
| + | |||
| + | == Motor | ||
| + | |||
| + | http:// | ||
| + | |||
| + | 1,000 N engine (enough to overcome rocket weight) | ||
| + | |||
| + | == Launch | ||
| + | |||
| + | The upward force is 216N. | ||
| + | |||
| + | The motor runs for 1 second. | ||
| + | |||
| + | |||
| + | == Questions | ||
| + | |||
| + | What is the speed of the vehicle? | ||
| + | |||
| + | 216N * 1s = 216 kg m/s (Unit of momentum) | ||
| + | |||
| + | 216kg m/s / 80 kg = 2.7m/s | ||
| + | |||
| + | What is the altitude of the vehicle? | ||
| + | |||
| + | position = acceleration * time^2 / 2 (from two rounds of integration) | ||
| + | |||
| + | 2.7 * 1^2 / 2 = 1.45m | ||
| + | |||