Challenge AMSO High Speed Reentry

Veterok

Veterok

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After launching at the planned time, and the crew of Apollo 16 changed their minds about their destination, and went for a Venus flyby instead. Now after a year and half in space they're almost home, they just need to re-enter... at over 14km/s.

Requires AMSO http://www.acsoft.ch/AMSO/amso.html
Make any adjustments you want, then eject the service module by pressing Ctrl+J, then J.

For the full flight just launch the Apollo 16 scenario in AMSO and complete your TVI by the end of the day.

(For an extra challenge I think you can line up a Mars flyby on the way back.)
 

Attachments

accepted.jpg


I'll try the full flight...
 
I just finished an Apollo 16 EVEEJSJE mission. But I need to go back and redo the last Jupiter flyby, I don't think re-entering on Earth at 22km/s is possible.
:cheers:
 
Veterok said:
I just finished an Apollo 16 EVEEJSJE mission. But I need to go back and redo the last Jupiter flyby, I don't think re-entering on Earth at 22km/s is possible.
:cheers:
Click to expand...

Either that or try aerobreaking in the Earth's atmosphere if you have the propellant left to do it. On the first past, go just deep enough to lose enough velocity to get you into a highly elliptical orbit and then drop a little more velocity with each pass until you are able to safely re-enter.
 
That's what I was trying to do, but I can't get below escape velocity without burning up. It took me about 20 tries to do it at 14km/s, I doubt it can be done at 22, but I'd love to see someone prove me wrong!
 
I tried a little too late - the SM seperated during the reentry. However, I did observe that the CM would skip out of the atmosphere into an elliptical "orbit" that takes it back into the atmosphere...
 
You can change the AOA to apply negative lift to keep the capsule down around 50km. Go much lower before you scrub off speed and you'll burn up.
 
I don't have the AMSO loaded but thought I would play with trajectories to see if a tour could be done with less encounter speed back at Earth. Found a tour of EVEEJSE with final Earth encounter speed of around 13.3 km/s. The TransX plan is in this deltaglider scenario set up a couple of minutes before the Apollo 16 launch. Haven't flown it but it looks fairly straightforward.
[edit] Noticed that in moving the launch time to actual time the date of eject was a bit off. I repaired this error and cleaned up the initial eject values with cleanup also of all slings. The repaired scenario is below the first one.

Code: 
BEGIN_DESC
Trajectory for imaginary Apollo 16 mutiny to fly to Venus Earth Earth Jupiter Saturn Earth with encounter speed at Earth of between 13 and 14 Km/s.
END_DESC

BEGIN_ENVIRONMENT
  System Sol
  Date MJD 41423.6608966608
END_ENVIRONMENT

BEGIN_FOCUS
  Ship 3
END_FOCUS

BEGIN_CAMERA
  TARGET 3
  MODE Cockpit
  FOV 60.00
END_CAMERA

BEGIN_MFD Left
  TYPE User
  MODE TransX
  Ship  3
  FNumber 13
  Int 1
  Orbit True
  Vector  5585148.10197 2716663.56664 1419739.73385
  Vector  -16.1872997656 -162.279300156 374.200084881
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END_MFD

BEGIN_MFD Right
  TYPE User
  MODE TransX
END_MFD

BEGIN_SHIPS
3:DeltaGlider
  STATUS Landed Earth
  BASE Cape Canaveral:1
  POS -80.6758964 28.5227640
  HEADING 75.00
  RCSMODE 0
  AFCMODE 7
  PRPLEVEL 0:1.000000 1:1.000000
  NAVFREQ 0 524 84 114
  XPDR 6
  GEAR 1 1.0000
  PSNGR 2 3 4
  TRIM 1.000000
  AAP 0:0 0:0 0:0
END
END_SHIPS

BEGIN_VistaBoost
END

Repaired scenario:
Code: 
BEGIN_DESC
Trajectory for imaginary Apollo 16 mutiny to fly to Venus Earth Earth Jupiter Saturn then Earth. Final encounter speed of around 13 km/sec.
END_DESC

BEGIN_ENVIRONMENT
  System Sol
  Date MJD 41423.6630600003
END_ENVIRONMENT

BEGIN_FOCUS
  Ship 3
END_FOCUS

BEGIN_CAMERA
  TARGET 3
  MODE Cockpit
  FOV 60.00
END_CAMERA

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Plan
0 0
Plan
0 2
Select Minor
 0 None
Manoeuvre mode
0 0
Base Orbit
0 0
Prograde vel.
 0  0
Man. date
 0  41423.6630459
Outward vel.
 0  0
Ch. plane vel.
 0  0
Intercept with
0 0
Orbits to Icept
0 0
Graph projection
0 0
Scale to view
0 1
Advanced
0 0
Velocity.
 0  0
Outward angle
 2  0.478742766625
Inc. angle
 0  -0.0703507314894
Inherit Vel.
0 0
Eject date
 0  43995.5615723
Finvars
  Finish BaseFunction
  Int 4
  Orbit True
  Vector  492162732440 -22680307755.6 159618223220
  Vector  -8021.89290963 370.719326393 -2625.51285925
  Double  3.79311866084e+016
  Double  44256.6703376
  Handle Saturn
  Handle NULL
  Handle NULL
Select Target
 0 Escape
Autoplan
0 0
Plan type
0 1
Plan
0 0
Plan
0 1
Plan
0 0
Select Minor
 0 None
Manoeuvre mode
0 0
Base Orbit
0 0
Prograde vel.
 0  0
Man. date
 0  41423.6630365
Outward vel.
 0  0
Ch. plane vel.
 0  0
Intercept with
0 0
Orbits to Icept
0 0
Graph projection
0 0
Scale to view
0 0
Advanced
0 0
View Orbit
0 0
Finvars
  Finish BaseFunction
  Int 3
  Orbit True
  Vector  -1.3847326649e+012 62028886910.4 -395872879933
  Vector  -5589.24932977 175.440440044 -5937.1534158
  Double  1.32750371142e+020
  Double  44962.8214351
  Handle Sun
  Handle Saturn
  Handle Earth
Select Target
 0 Earth
Autoplan
0 0
Plan type
0 2
Plan
0 0
Plan
0 0
Plan
0 2
Select Minor
 0 None
Manoeuvre mode
0 0
Base Orbit
0 0
Prograde vel.
 0  0
Man. date
 0  41423.6630351
Outward vel.
 0  0
Ch. plane vel.
 0  0
Intercept with
0 0
Orbits to Icept
0 0
Graph projection
0 0
Scale to view
0 1
Advanced
0 0
Velocity.
 0  0
Outward angle
 3  2.21906327273
Inc. angle
 0  0.0231812885921
Inherit Vel.
0 0
Eject date
 0  44962.8214351
Finvars
  Finish BaseFunction
  Int 5
  Orbit True
  Vector  3363134115.4 -1769076944.94 -8470511235.4
  Vector  -4640.00355904 2398.73209167 12186.7706586
  Double  3.98600439969e+014
  Double  51132.7617207
  Handle Earth
  Handle NULL
  Handle NULL
Select Target
 0 None
Autoplan
0 0
Plan type
0 1
Plan
0 0
Plan
0 2
Plan
0 0
Select Minor
 0 None
Manoeuvre mode
0 0
Base Orbit
0 0
Prograde vel.
 0  0
Man. date
 0  41423.6630599
Outward vel.
 0  0
Ch. plane vel.
 0  0
Intercept with
0 0
Orbits to Icept
0 0
Graph projection
0 0
Scale to view
0 0
Advanced
0 0
Draw Base
0 0
Finvars
  Finish BaseFunction
END_MFD

BEGIN_MFD Right
  TYPE User
  MODE TransX
END_MFD

BEGIN_SHIPS
3:DeltaGlider
  STATUS Landed Earth
  BASE Cape Canaveral:1
  POS -80.6758964 28.5227640
  HEADING 75.00
  RCSMODE 0
  AFCMODE 7
  PRPLEVEL 0:1.000000 1:1.000000
  NAVFREQ 0 524 84 114
  XPDR 6
  GEAR 1 1.0000
  PSNGR 2 3 4
  TRIM 1.000000
  AAP 0:0 0:0 0:0
END
END_SHIPS

BEGIN_VistaBoost
END


---------- Post added at 03:11 PM ---------- Previous post was at 08:27 AM ----------

I went ahead and flew it. The arrival back at Earth had an encounter speed of about 11km/s which translated to a bit over 15 km/sec at the Pe. Here's a screen cap of arriving. (click to enlarge)

What was interesting was on the initial departure from Earth, the trajectory on takeoff had a great view of the moon Venus and Saturn lumped together, and on the eject from LEO, the trajectory had me going past the moon fairly close to it. I was worried it would mess up the plan to Venus but it was far enough to cause minimal damage to the course.
 
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