orbitalmechanics
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| Both sides previous revisionPrevious revisionNext revision | Previous revision | ||
| orbitalmechanics [2011/08/25 21:13] – donpdonp | orbitalmechanics [2024/01/31 04:08] (current) – external edit 127.0.0.1 | ||
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| Line 5: | Line 5: | ||
| 80kg (175 lbs) | 80kg (175 lbs) | ||
| - | 80k in earth' | + | 80kg in earth' |
| == Motor | == Motor | ||
| Line 11: | Line 11: | ||
| http:// | http:// | ||
| - | Size J - 1,000 N*s (enough to overcome | + | 1,000 N engine |
| - | == Questions | + | == Launch |
| - | Given that the motor has run for one second, | + | The upward force is 216N. |
| + | |||
| + | The motor runs for 1 second. | ||
| + | |||
| + | |||
| + | == Questions | ||
| What is the speed of the vehicle? | 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? | What is the altitude of the vehicle? | ||
| + | |||
| + | position = acceleration * time^2 / 2 (from two rounds of integration) | ||
| + | |||
| + | 2.7 * 1^2 / 2 = 1.45m | ||
| + | |||
orbitalmechanics.1314306790.txt.gz · Last modified: 2024/01/31 04:08 (external edit)