Space Shuttle Ultra 4.2 released!!!

[DaveS]

This is the OMS-2/ON-ORBIT OMS BURN cue-card used by the CDR/PLT/MS2 to set up and monitor OMS burns:

OMS GIMBAL ANGLES are ITEMs 5 through 7. Time of Ignition (TIG) are ITEMs 10 through 12 in Mission Elapsed Time (MET). PEG7 Delta V targets are ITEMs 17 through 19 in feet/second (fps). To load the targets enter ITEM 22 EXEC. If happy with targets, ITEM 23 EXEC to initialize the burn timer. at TIG-15 EXEC will flash, just hit EXEC to confirm the burn.

 

[Wolf]

Sorry guys, maybe you have checked that already; I've noticed the air data probes look partially deployed (SSU 4.2).

 

[Donamy]

What are the xyz coordinates of the payload bay ?

 

[DaveS]

What are the xyz coordinates of the payload bay ?

Here's the coordinates from AC3D: 0.0, -1.39831, 0.46303

 

[Donamy]

I mean the parent attachments.

 

[DaveS]

I mean the parent attachments.

OK, I see. Page 9 of the SSU 4.2 manual has the locations of the various attachment points on the orbiter. The number next to each dot on the figures represent its attachment point number.

 

[Donamy]

And where can I find that ?

Never mind. Found it.

 

[Donamy]

Having a problem with the SRMS. I grapple a vessel move it around alittle and it seems ok. But soon it just continues to rolls around the attachment point.anyone else have this issue ?

 

[GLS]

Having a problem with the SRMS. I grapple a vessel move it around alittle and it seems ok. But soon it just continues to rolls around the attachment point.anyone else have this issue ?

I just ran the "Payload Latch Test" scenario at 10x and moved the arm in several axis at the same time and didn't notice any (large) motion between the EE and the MPLM.

 

[Donamy]

Try it again, and switch between Orbiter ans EE frame. Do it for at least 3 or 4 min.
rot and trans.

 

[DaveS]

Try it again, and switch between Orbiter ans EE frame. Do it for at least 3 or 4 min.
rot and trans.

By Orbiter and EE frame do you mean camera views?

 

[GLS]

Try it again, and switch between Orbiter ans EE frame. Do it for at least 3 or 4 min.
rot and trans.

As soon as I finish updating the projects.

By Orbiter and EE frame do you mean camera views?

I think he means RMS motion frame.

 

[Donamy]

Yes to the motion frame.

 

[Donamy]

The first pic is after the RMS, has been maneuvered to position for ingress, to the PFR on the RMS. The EE attachment should be attached to the bottom of the wrist, where it was when the maneuver was started. The second pic is where the PFR is, when the current scenario is restarted. I changed focus to the Discovery, then restarted the current scenario, and the PFR snaps to the correct position.

 

[GLS]

The first pic is after the RMS, has been maneuvered to position for ingress, to the PFR on the RMS. The EE attachment should be attached to the bottom of the wrist, where it was when the maneuver was started. The second pic is where the PFR is, when the current scenario is restarted. I changed focus to the Discovery, then restarted the current scenario, and the PFR snaps to the correct position.

You wouldn't be using SSU 4.2 in Orbiter 2016? :hmm:

 

[Donamy]

err ...Yes I am.

 

[GLS]

err ...Yes I am.

The way the attachments were handled in 2010 didn't work in 2016, as you see...