Spacecrafts for Celestia
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Topic authortoutatis
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Mars Express add-on by toutatis... (orbiter only... there is no data at HORIZONS for interplanetary cruise stage for this spacecraft... but model with a lander also included)...
- Attachments
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- Mars Express.7z
- (5.09 MiB) Downloaded 227 times
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Topic authortoutatis
- Posts: 744
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Correction for SSC-file... it's again about demensions... lol
Code: Select all
"Mars Express" "Sol/Mars"
{
Class "spacecraft"
Mesh "Mars Express-os1.cmod"
Radius 0.006
Beginning "2003 12 30 12:10:00"
Ending "2005 06 14 18:00:00"
OrbitFrame
{
EclipticJ2000 { Center "Sol/Mars" }
}
SampledTrajectory
{
Source "MEX-Orbiter-1.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars/Mars Express"
Primary
{
Axis "-x"
RelativePosition
{
Observer "Sol/Mars/Mars Express"
Target "Sol/Earth"
}
}
Secondary
{
Axis "y"
RelativeVelocity
{
Observer "Sol/Mars/Mars Express"
Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.00
}
}
"Mars Express(+M)" "Sol/Mars"
{
Class "spacecraft"
Mesh "Mars Express-os2.cmod"
Radius 0.02
Timeline
[
{
Beginning "2005 06 14 18:00:00"
Ending "2005 08 20 00:00:00"
OrbitFrame
{
EclipticJ2000 { Center "Sol/Mars" }
}
SampledTrajectory
{
Source "MEX-Orbiter-2.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars/Mars Express(+M)"
Primary
{
Axis "-x"
RelativePosition
{
Observer "Sol/Mars/Mars Express(+M)"
Target "Sol/Earth"
}
}
Secondary
{
Axis "y"
RelativeVelocity
{
Observer "Sol/Mars/Mars Express(+M)"
Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.00
}
}
{
Ending "2022 01 01 00:00:00"
OrbitFrame
{
EclipticJ2000 { Center "Sol/Mars" }
}
EllipticalOrbit
{
Epoch 2453602.5 # 2005 Aug 20 00:00:00
Period 0.279800673461397
SemiMajorAxis 8590.77373382230644
Eccentricity 0.5714531044319604
Inclination 65.31211882427604
AscendingNode 223.1629732348163
ArgOfPericenter 14.84817736451892
MeanAnomaly 300.4891851886892
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars/Mars Express(+M)"
Primary
{
Axis "-x"
RelativePosition
{
Observer "Sol/Mars/Mars Express(+M)"
Target "Sol/Earth"
}
}
Secondary
{
Axis "y"
RelativeVelocity
{
Observer "Sol/Mars/Mars Express(+M)"
Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.00
}
}
]
}
Last edited by toutatis on 01.06.2019, 19:38, edited 1 time in total.
- SpaceFanatic64
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- gironde
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beautiful achievement
here are informations of ESA about Spice support (Mars Express Mex, Venus Express Vex, Rosetta Ros, and other coming soon)
https://www.cosmos.esa.int/web/psa/ancillary-data
Added after 46 minutes 40 seconds:
Hey Toutatis
for a radius of 6 meters (body + solar cells), write Radius 0.006 and not 0.0006
here are informations of ESA about Spice support (Mars Express Mex, Venus Express Vex, Rosetta Ros, and other coming soon)
https://www.cosmos.esa.int/web/psa/ancillary-data
Added after 46 minutes 40 seconds:
Hey Toutatis
Correction for SSC-file... it's again about demensions... lol
for a radius of 6 meters (body + solar cells), write Radius 0.006 and not 0.0006
-
Topic authortoutatis
- Posts: 744
- Joined: 24.02.2018
- Age: 55
- With us: 6 years 9 months
- Location: Almaty, Kazakhstan
for a radius of 6 meters (body + solar cells), write Radius 0.006 and not 0.0006
OMG... again.... Thanks gironde!
Corrected already...
Added after 7 minutes 17 seconds:
here are informations of ESA about Spice support (Mars Express Mex, Venus Express Vex, Rosetta Ros, and other coming soon)
https://www.cosmos.esa.int/web/psa/ancillary-data
It's interesting...
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Topic authortoutatis
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USS Toutatis... ... will start journey to Jupiter system during this month... to enter in orbit around Europa... (need to practice in modeling and making xyzv-trajectories...)
- Attachments
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- USS Toutatis.7z
- (771.77 KiB) Downloaded 195 times
- Lafuente_Astronomy
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toutatis wrote:USS Toutatis... ... will start journey to Jupiter system during this month... to enter in orbit around Europa... (need to practice in modeling and making xyzv-trajectories...)
Bon Voyage to the King Planet my friend!
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- SpaceFanatic64
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