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Each daily launch window for STS-49 was a maximum of 53 minutes long with the shortest being 47 minutes long.

Here's another one showing Atlantis undergoing Orbiter Maintenance Down Period(OMDP)-J1 in Palmdale, CA, between October 1992 and May 1994: Additions to the orbiter included the improved nosewheel steering system, improved APUs, the drag chute modification to the vertical stabilizer, lightweight...

Rockwell Intl film showing STA-099(would later be converted into OV-099, Challenger) payload bay doors being attached to the midbody with a showing of OV-102 (Columbia) at the end, the least complete orbiter on the right: https://catalog.archives.gov/id/70180522

Just a complete shot in the dark here, but do you have a plug-in called "Attachment Manager" active? If so, try disabling it.

On the video tab where it's says Full Screen Mode, select Full Screen Window. True Full Screen doesn't support anything that makes Orbiter lose focus.

AXM Model's Shuttle Reference: https://axmpaperspacescalemodels.com/index.php/shuttle-reference/

It was all SWT until STS-6 which introduced the LWT, then back SWT for STS-7. SLWT was introduced on STS-91, the last Shuttle/Mir mission. STS-99 used a LWT as did STS-107. STS-87 was the first launch to do the Roll To Heads Up (RTHU) during the second stage launch.

See my additional reply, it was without the MFDs from the start. Forgot that I deleted the blocks in the scenario last night.

Another detail is this happen with the MDUs turned completely off, no MFD blocks in the scenario, only the VC block.

Another day, another crash, this time here: https://www.dropbox.com/scl/fi/nuqk6ca77j25yqsqwt07c/VS_debugger_D3D9Client4.jpg?rlkey=k77oknl6j0xgw7dagjgpfu7ke&dl=0 Details are: Unpaused, 0.1x time accel, exterior camera view, pre-launch at T-8:47.8, mission STS-109, so OV-102 8th mod, PLB liner...

Another crash, this time on the pad, while paused, same error as earlier though: https://www.dropbox.com/scl/fi/p37tmzmmr59n48i4sf2b8/Orbiter_D3D9Client_SSV_error_paused.jpg?rlkey=jbu2h7hd2m994u6ja4qdzzr5j&dl=0 Line 299 of DrawAPI.h is the end of the following bit code: inline FVECTOR3...

Well, so far both SLS Core Stages and ICPS's have been flawless. The hydrogen leaks are a Ground Support Equipment (GSE) problem, not a flight hardware problem. The helium problem encountered with the Artemis-1 ICPS was that a ground-side seal got blown into the ICPS helium system and prevented...

Not it wasn't. That was never the plan. SLS never had that capability, it was always short hence the requirement of the Gateway Station in NHRO for Orion to dock to. Gateway would serve as hibernation point for Orion while the crew went to the lunar surface and back again in the HLS lander...

Click the Advanced button and make sure Full Scene is selected under Reflections and Custom camera settings.

And here's another: https://www.dropbox.com/scl/fi/h8z4o15rtlsfeor861yz5/VS_debugger_D3D9Client3.jpg?rlkey=gb4pok5qptbiugqipwp6iqv7w&dl=0 https://www.dropbox.com/scl/fi/4mjp8vzc8j1blkphy30i1/VS_debugger_D3D9Client3A.jpg?rlkey=7kyabmtv628jjewn0oux37by2&dl=0...

Different error this time: https://www.dropbox.com/scl/fi/9gdftg0fn7d615z6il3cj/VS_debugger_D3D9Client2.jpg?rlkey=ugxl3e0zrrrm74rwljhk26wnu&dl=0 https://www.dropbox.com/scl/fi/9gdftg0fn7d615z6il3cj/VS_debugger_D3D9Client2.jpg?rlkey=ugxl3e0zrrrm74rwljhk26wnu&dl=0...

Here's the call stack window: https://www.dropbox.com/scl/fi/duza1hyfaj6uhmi7g8qh5/VS_debugger_D3D9Client_call_stack.jpg?rlkey=e856kn4fqs28p604gpf8x8oiv&dl=0

How do I check for that?

CTD and caught by the debugger: https://www.dropbox.com/scl/fi/ejrfentjpfaftfvllywbx/VS_dubugger_SSV_CTD_Run3.jpg?rlkey=ygolvlkq3rafv886f8irn6h8q&dl=0

That yielded complete success in the build phase I've replaced the original release files with the newly built debug versions.