- Joined
- Feb 4, 2008
- Messages
- 9,434
- Reaction score
- 689
- Points
- 203
As far as the full stack aerodynamics go, here's what we got right now:
1st stage(SRB+ET+Orbiter):
SetCrossSections(_V(668.94, 676.94, 258.97));
SetRotDrag(_V(0.7, 0.1, 0.3));
SetPMI(_V(249.62, 239.97, 67.43));
2nd stage(ET+Orbiter):
SetCrossSections(_V(303.91, 422.33, 153.51));
SetRotDrag(_V(0.7, 0.1, 0.3));
SetPMI(_V(131.82, 131.49, 59.28));
And I really think that we should focus on getting the basic SSV (Space Shuttle Vehicle, the "stack name" for the fully assembled vehicle) done first. We have a viable roadmap, let's stick to it.
1st stage(SRB+ET+Orbiter):
SetCrossSections(_V(668.94, 676.94, 258.97));
SetRotDrag(_V(0.7, 0.1, 0.3));
SetPMI(_V(249.62, 239.97, 67.43));
2nd stage(ET+Orbiter):
SetCrossSections(_V(303.91, 422.33, 153.51));
SetRotDrag(_V(0.7, 0.1, 0.3));
SetPMI(_V(131.82, 131.49, 59.28));
And I really think that we should focus on getting the basic SSV (Space Shuttle Vehicle, the "stack name" for the fully assembled vehicle) done first. We have a viable roadmap, let's stick to it.