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| author | Baitinq <you@example.com> | 2022-02-10 23:35:08 +0000 |
|---|---|---|
| committer | Baitinq <you@example.com> | 2022-02-10 23:35:08 +0000 |
| commit | 4da2b48e4e6837047b4076e9ec388c1a8d00afa3 (patch) | |
| tree | 9e2f91afe8c6a78ba1a39b425e9abf46220c781a /rocket.py | |
| parent | Fixed heading calculation by using atan2 (diff) | |
| download | OSLS-4da2b48e4e6837047b4076e9ec388c1a8d00afa3.tar.gz OSLS-4da2b48e4e6837047b4076e9ec388c1a8d00afa3.tar.bz2 OSLS-4da2b48e4e6837047b4076e9ec388c1a8d00afa3.zip | |
Started preparation to implement proper altitude calculations and gravity
Diffstat (limited to 'rocket.py')
| -rw-r--r-- | rocket.py | 2 |
1 files changed, 2 insertions, 0 deletions
diff --git a/rocket.py b/rocket.py index 962678b..fb8ea7c 100644 --- a/rocket.py +++ b/rocket.py @@ -37,5 +37,7 @@ class Rocket(): def s_drag_coefficient(self): return self.top_stage().drag_coefficient + #TODO: IMPLEMENT rocket_x_drag_coefficient() that adds the x drag coefficient of all stages, same with cross sectional area + def __str__(self): return "eue" \ No newline at end of file |