Spacecrafts for Celestia
- Anthony_B_Russo10
- Moderator
- Posts: 530
- Joined: 03.07.2018
- Age: 18
- With us: 2 years 8 months
- Location: Tallahassee, Florida, US
But English can be a pain when you have to learn words that you will never use in normal day to day life.
Anthony B. Russo, I like Pluto. Mod of the Celestia subreddit: https://www.reddit.com/r/Celestiasoftware/
I have over 30 computers, trying to list them here would be a pain.
I have over 30 computers, trying to list them here would be a pain.
-
Topic authortoutatis
- Posts: 667
- Joined: 24.02.2018
- Age: 52
- With us: 3 years
- Location: Almaty, Kazakhstan
a small changes for GRAIL and MRO add-ons... for MRO, HiRISE cam direction to Mars, after arriving to the red planet... in the picture MRO several minutes ago over Nord pole of planet... when we use XYZV-trajectories we can know where spacecraft in the real moment of time...
- Attachments
-
MRO_SSC.7z
- (1.01 KiB) Downloaded 121 times
-
GRAIL_SSC&XYZV.7z
- (237.19 KiB) Downloaded 109 times
-
Topic authortoutatis
- Posts: 667
- Joined: 24.02.2018
- Age: 52
- With us: 3 years
- Location: Almaty, Kazakhstan
* Mars Atmosphere and Volatile Evolution (MAVEN) * the full XYZV-trajectory by data from HORIZONS... Timeline...
- Attachments
-
MAVEN (USA NASA).7z
- (13.15 MiB) Downloaded 131 times
-
Topic authortoutatis
- Posts: 667
- Joined: 24.02.2018
- Age: 52
- With us: 3 years
- Location: Almaty, Kazakhstan
just added COSPAR ID in SSC-file for MRO...
Code: Select all
"Mars Reconnaissance Orbiter:MRO:2005-029A" "Sol"
{
Class "spacecraft"
Mesh "mars-reconnaissance-orbiter.cmod"
Radius 0.0065
Timeline
[
{
Beginning 2453595.029166667 #
Ending 2453805.0 #
OrbitFrame
{
EclipticJ2000 { Center "Sol" }
}
SampledTrajectory
{
Source "MRO-Sun.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars Reconnaissance Orbiter"
Primary
{
Axis "x"
RelativePosition
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol"
}
}
Secondary
{
Axis "-z"
RelativeVelocity
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol"
}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2453896.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars1.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars Reconnaissance Orbiter"
Primary
{
Axis "-y"
RelativePosition
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
Secondary
{
Axis "-z"
RelativeVelocity
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2453988.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars2.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars Reconnaissance Orbiter"
Primary
{
Axis "-y"
RelativePosition
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
Secondary
{
Axis "-z"
RelativeVelocity
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2454079.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars3.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars Reconnaissance Orbiter"
Primary
{
Axis "-y"
RelativePosition
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
Secondary
{
Axis "-z"
RelativeVelocity
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2454169.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars4.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars Reconnaissance Orbiter"
Primary
{
Axis "-y"
RelativePosition
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
Secondary
{
Axis "-z"
RelativeVelocity
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2454261.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars5.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars Reconnaissance Orbiter"
Primary
{
Axis "-y"
RelativePosition
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
Secondary
{
Axis "-z"
RelativeVelocity
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2454353.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars6.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars Reconnaissance Orbiter"
Primary
{
Axis "-y"
RelativePosition
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
Secondary
{
Axis "-z"
RelativeVelocity
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2454444.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars7.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars Reconnaissance Orbiter"
Primary
{
Axis "-y"
RelativePosition
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
Secondary
{
Axis "-z"
RelativeVelocity
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2454535.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars8.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars Reconnaissance Orbiter"
Primary
{
Axis "-y"
RelativePosition
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
Secondary
{
Axis "-z"
RelativeVelocity
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2454627.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars9.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars Reconnaissance Orbiter"
Primary
{
Axis "-y"
RelativePosition
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
Secondary
{
Axis "-z"
RelativeVelocity
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2454719.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars10.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars Reconnaissance Orbiter"
Primary
{
Axis "-y"
RelativePosition
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
Secondary
{
Axis "-z"
RelativeVelocity
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2454810.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars11.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars Reconnaissance Orbiter"
Primary
{
Axis "-y"
RelativePosition
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
Secondary
{
Axis "-z"
RelativeVelocity
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2454900.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars12.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars Reconnaissance Orbiter"
Primary
{
Axis "-y"
RelativePosition
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
Secondary
{
Axis "-z"
RelativeVelocity
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2454992.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars13.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars Reconnaissance Orbiter"
Primary
{
Axis "-y"
RelativePosition
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
Secondary
{
Axis "-z"
RelativeVelocity
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2455084.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars14.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars Reconnaissance Orbiter"
Primary
{
Axis "-y"
RelativePosition
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
Secondary
{
Axis "-z"
RelativeVelocity
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2455175.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars15.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars Reconnaissance Orbiter"
Primary
{
Axis "-y"
RelativePosition
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
Secondary
{
Axis "-z"
RelativeVelocity
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2455265.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars16.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars Reconnaissance Orbiter"
Primary
{
Axis "-y"
RelativePosition
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
Secondary
{
Axis "-z"
RelativeVelocity
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2455357.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars17.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars Reconnaissance Orbiter"
Primary
{
Axis "-y"
RelativePosition
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
Secondary
{
Axis "-z"
RelativeVelocity
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2455449.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars18.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars Reconnaissance Orbiter"
Primary
{
Axis "-y"
RelativePosition
{
Observer "Sol/Mars Reconnaissance Orbiter"
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}
}
Secondary
{
Axis "-z"
RelativeVelocity
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}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2455540.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars19.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars Reconnaissance Orbiter"
Primary
{
Axis "-y"
RelativePosition
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
Secondary
{
Axis "-z"
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Target "Sol/Mars"
}
}
}
}
FixedRotation
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Period 0.0
}
}
{
Ending 2455630.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars20.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
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Primary
{
Axis "-y"
RelativePosition
{
Observer "Sol/Mars Reconnaissance Orbiter"
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}
}
Secondary
{
Axis "-z"
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Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2455722.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
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{
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DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
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Primary
{
Axis "-y"
RelativePosition
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Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
Secondary
{
Axis "-z"
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Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2455814.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars22.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
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Primary
{
Axis "-y"
RelativePosition
{
Observer "Sol/Mars Reconnaissance Orbiter"
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}
}
Secondary
{
Axis "-z"
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Target "Sol/Mars"
}
}
}
}
FixedRotation
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Period 0.0
}
}
{
Ending 2455905.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
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{
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Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
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{
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}
Secondary
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}
}
}
}
FixedRotation
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Period 0.0
}
}
{
Ending 2455996.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
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{
Source "MRO-Mars24.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
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Primary
{
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}
Secondary
{
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}
}
}
}
FixedRotation
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Period 0.0
}
}
{
Ending 2456088.5 #
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{
EclipticJ2000 {Center "Sol/Mars"}
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}
BodyFrame
{
TwoVector
{
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{
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}
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Axis "-z"
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}
}
}
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FixedRotation
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Period 0.0
}
}
{
Ending 2456180.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
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{
Source "MRO-Mars26.xyzv"
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Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
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{
Axis "-y"
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}
Secondary
{
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}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2456271.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars27.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars Reconnaissance Orbiter"
Primary
{
Axis "-y"
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{
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}
}
Secondary
{
Axis "-z"
RelativeVelocity
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Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2456361.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars28.xyzv"
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Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
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{
Axis "-y"
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{
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}
}
Secondary
{
Axis "-z"
RelativeVelocity
{
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Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2456453.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars29.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars Reconnaissance Orbiter"
Primary
{
Axis "-y"
RelativePosition
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
Secondary
{
Axis "-z"
RelativeVelocity
{
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Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2456545.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars30.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars Reconnaissance Orbiter"
Primary
{
Axis "-y"
RelativePosition
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
Secondary
{
Axis "-z"
RelativeVelocity
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.0
}
}
{
Ending 2456636.5 #
OrbitFrame
{
EclipticJ2000 {Center "Sol/Mars"}
}
SampledTrajectory
{
Source "MRO-Mars31.xyzv"
DoublePrecision true
Interpolation "cubic"
}
BodyFrame
{
TwoVector
{
Center "Sol/Mars Reconnaissance Orbiter"
Primary
{
Axis "-y"
RelativePosition
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
Secondary
{
Axis "-z"
RelativeVelocity
{
Observer "Sol/Mars Reconnaissance Orbiter"
Target "Sol/Mars"
}
}
}
}
FixedRotation
{
Period 0.0
}
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-
Topic authortoutatis
- Posts: 667
- Joined: 24.02.2018
- Age: 52
- With us: 3 years
- Location: Almaty, Kazakhstan
* Lunar Reconnaissance Orbiter (LRO) *... the full xyzv-trajectory by data from HORIZONS... Timeline... the model of LRO by BrianJ was a bit modernized, smoothed some elements...
Added after 15 minutes 6 seconds:
..................
Added after 15 minutes 6 seconds:
..................
- Attachments
-
Lunar Reconnaissance Orbiter (USA NASA).7z
- (27.96 MiB) Downloaded 137 times
-
Topic authortoutatis
- Posts: 667
- Joined: 24.02.2018
- Age: 52
- With us: 3 years
- Location: Almaty, Kazakhstan
Just found an errors in the files from HORIZONS system, when created a xyzv-trajectory for Mars Express spacecraft... that brings a visual defects in Celestia when we want observe trajectory... these errors I found in timespan between 08:00:00 and 09:00:00 December 30, 2003... but because it happened when MEX was in Apocenter of the first it orbit around Mars to solve the problem I just deleted the data from with errors... and now all okay...
in the pictures you can see a MEX "making a working orbit"...
Added after 9 minutes 49 seconds:
You can see that MEX made a maneuver close to Apocenter to change inclination of orbit... such maneuvers better to do close to apocenter...
in the pictures you can see a MEX "making a working orbit"...
Added after 9 minutes 49 seconds:
You can see that MEX made a maneuver close to Apocenter to change inclination of orbit... such maneuvers better to do close to apocenter...
- Sirius_Alpha
- Posts: 110
- Joined: 21.03.2019
- With us: 1 year 11 months
I'm not sure I understand exactly what you mean. Are you saying that because the inclination change was performed at apoastron, you think the data is suspecft?
If so, it turns out inclination changes occur best at lower orbital velocities. Inclination changes at apoastron are much more fuel-efficient since the components of the velocity vector are smaller.
If so, it turns out inclination changes occur best at lower orbital velocities. Inclination changes at apoastron are much more fuel-efficient since the components of the velocity vector are smaller.
Exoplanet nerd. I maintain a monthly-updated exoplanet catalogue here:
https://celestia.space/forum/viewtopic.php?f=23&t=18705
https://celestia.space/forum/viewtopic.php?f=23&t=18705
-
Topic authortoutatis
- Posts: 667
- Joined: 24.02.2018
- Age: 52
- With us: 3 years
- Location: Almaty, Kazakhstan
Yes, Sirius_Alpha... that is right...inclination changes occur best at lower orbital velocities. Inclination changes at apoastron are much more fuel-efficient since the components of the velocity vector are smaller.
I'm not sure I understand exactly what you mean. Are you saying that because the inclination change was performed at apoastron, you think the data is suspecft?
I mean, there I found real errors in data I downloaded...
- SpaceFanatic64
- Posts: 405
- Joined: 16.08.2018
- Age: 15
- With us: 2 years 6 months
- Location: Southern California
- SpaceFanatic64
- Posts: 405
- Joined: 16.08.2018
- Age: 15
- With us: 2 years 6 months
- Location: Southern California
https://nasa3d.arc.nasa.gov/detail/GeoTail The Geotail spacecraft. I suggested this a very long time ago, but nothing ever came out of it.
Follower of the "Celestia Origin" project
Graphics Card: ATI Radeon 3000 Graphics
Graphics Card: ATI Radeon 3000 Graphics
-
Topic authortoutatis
- Posts: 667
- Joined: 24.02.2018
- Age: 52
- With us: 3 years
- Location: Almaty, Kazakhstan
* Cassini-Huygens *... In this add-on, was used only two modernized models, the Cassini spacecraft and the Huygens probe... I combined them through a SSC-file... a smooth separation of the parts of the spacecraft was not made because of a "bad" data for Huygens by ESA...
- Attachments
-
Cassini-Huygens (USA JPL NASA_EU ESA).7z
- (33.73 MiB) Downloaded 124 times
Last edited by toutatis on 19.09.2019, 02:57, edited 1 time in total.