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Merge pull request #1300 from maxq519/Custom-Payloads
Add support for custom user-defined payloads in the Saturn 5/1B SLA, as well as an optional wide ELS-type SLA
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Original file line number | Diff line number | Diff line change |
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; === Configuration file for vessel class Saturn V === | ||
ClassName = sat5stg31wide | ||
MeshName = ProjectApollo/sat5stg31wide | ||
Size = 5.0 | ||
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Mass = 600 ; empty mass [kg] | ||
COG_OverGround = 2.0 | ||
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; === Atmospheric flight model === | ||
CW = 0.5 1.1 2 2.4 | ||
CrossSections = 32.75 34.75 8.35 | ||
RotResistance = 2.0 2.0 2.0 | ||
Inertia = 7.5 7.5 0.85 | ||
EnableFocus = FALSE |
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Original file line number | Diff line number | Diff line change |
---|---|---|
@@ -0,0 +1,14 @@ | ||
; === Configuration file for vessel class Saturn V === | ||
ClassName = sat5stg32wide | ||
MeshName = ProjectApollo/sat5stg32wide | ||
Size = 5.0 | ||
|
||
Mass = 600 ; empty mass [kg] | ||
COG_OverGround = 2.0 | ||
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||
; === Atmospheric flight model === | ||
CW = 0.5 1.1 2 2.4 | ||
CrossSections = 32.75 34.75 8.35 | ||
RotResistance = 2.0 2.0 2.0 | ||
Inertia = 15.35 15.35 2.85 | ||
EnableFocus = FALSE |
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@@ -0,0 +1,15 @@ | ||
; === Configuration file for vessel class Saturn V === | ||
ClassName = sat5stg33wide | ||
MeshName = ProjectApollo/sat5stg33wide | ||
Size = 5.0 | ||
|
||
Mass = 600 ; empty mass [kg] | ||
COG_OverGround = 2.0 | ||
|
||
; === Atmospheric flight model === | ||
CW = 0.5 1.1 2 2.4 | ||
CrossSections = 32.75 34.75 8.35 | ||
RotResistance = 2.0 2.0 2.0 | ||
Inertia = 15.35 15.35 2.85 | ||
EnableFocus = FALSE | ||
|
This file contains bidirectional Unicode text that may be interpreted or compiled differently than what appears below. To review, open the file in an editor that reveals hidden Unicode characters.
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Original file line number | Diff line number | Diff line change |
---|---|---|
@@ -0,0 +1,14 @@ | ||
; === Configuration file for vessel class Saturn V === | ||
ClassName = sat5stg34wide | ||
MeshName = ProjectApollo/sat5stg34wide | ||
Size = 5.0 | ||
|
||
Mass = 600 ; empty mass [kg] | ||
COG_OverGround = 2.0 | ||
|
||
; === Atmospheric flight model === | ||
CW = 0.5 1.1 2 2.4 | ||
CrossSections = 32.75 34.75 8.35 | ||
RotResistance = 2.0 2.0 2.0 | ||
Inertia = 15.35 15.35 2.85 | ||
EnableFocus = FALSE |
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