It's obviously in the nacelle. It can't fit into the 340' secondary hull and leave room for anything else (unless you have the brewery edition of the EnterpriseThe structure would definitely fit into the secondary hull (which could also be nicknamed the "antimatter nacelle" in this scenario) but what would explain its cylindrical design?
Could it run along the centreline of the secondary hull, behind the main dish structure?
Just for fun, I thought I would run some approximate measurements on the "nacelle room" from One Of Our Planets Is Missing:
http://tas.trekcore.com/gallery/thumbnails.php?album=44&page=15
http://tas.trekcore.com/gallery/thumbnails.php?album=3&page=7
As is not uncommon in TAS the scale is irregular, but can can assume the door is between 78" and 84" high
![]()
We see a total of 6 rows of those energy pipes in a sideways pan (not on Trekcore), but a total of 8 can be assumed from this shot:
![]()
Depending on the height of the door that Scott and Kirk first enter from, the whole room need not be more than 80 feet long by 35 feet high, certainly not more than 100 feet long.
The structure would definitely fit into the secondary hull (which could also be nicknamed the "antimatter nacelle" in this scenario) but what would explain its cylindrical design?
Could it run along the centreline of the secondary hull, behind the main dish structure?
It looks like someone just copied the interior of a 1930's dirigible framework for the TAS nacelle. Does it fit in the warp nacelle?
Also, the horizontal cylinder with the pipes is not on the center but shifted vertically down. That would suggest the vertical/angled pipes are not equal length.
As always with Trek, things that might be one thing if the episode was taken in isolation may not be that way when looking at the series as a wholeIt's obviously in the nacelle.
Well if we go by Scott's dialogue then this structure is the "antimatter engine" tentatively located in the secondary hull (AKA the antimatter nacelle). If the interior of the cylinder is 30' diameter then even allowing for 10' of machinery on the outside then that all easily fits into a secondary hull which even on a 947' Enterprise has a maximum diameter of around 90'The power tubes must connect to something beyond the 35-40' diameter room, like warp devices to generate the warp field. If these devices are ~10 thick plus a little gap to the outer skin thickness, we are at 60' diameter, the diameter of the nacelle.
Hardly a first on the Enterprise. The cylindrical nature of the room as a whole (centred on the the door) would still be at home in the secondary hull IMOAlso, the horizontal cylinder with the pipes is not on the center but shifted vertically down. That would suggest the vertical/angled pipes are not equal length.
Same thoughts on both dirigible and off-center tubes. There is a chance that the horizontal core tube and pipe spokes are in the center, and the walkway, door, tubular room and its wall panelling are off-center...i.e. a tube in a tube off-centered (A) or centered (B)?It looks like someone just copied the interior of a 1930's dirigible framework for the TAS nacelle. Does it fit in the warp nacelle?
Also, the horizontal cylinder with the pipes is not on the center but shifted vertically down. That would suggest the vertical/angled pipes are not equal length.
Same thoughts on both dirigible and off-center tubes. There is a chance that the horizontal core tube and pipe spokes are in the center, and the walkway, door, tubular room and its wall panelling are off-center...i.e. a tube in a tube off-centered (A) or centered (B)?
![]()
I'm really not fond of (A) if you're going to stick to the door-centred TAS design.Same thoughts on both dirigible and off-center tubes. There is a chance that the horizontal core tube and pipe spokes are in the center, and the walkway, door, tubular room and its wall panelling are off-center...i.e. a tube in a tube off-centered (A) or centered (B)?
![]()
Self-Sealing Stem Bolts?very big bolts
And I say, apply 60 years of jet engine mounting knowledge to the warp engines, which are supposed to mimic "quick change units". While I acknowledge the question of scale, jet engines use surprisingly few mount points to stay attached to planes and require none of the overbuilt internal support too often proposed for warp nacelles.
Here's a short video on the installation of an A-10 Warthog engine. (4:44 long. Relevant view at about 0:32.)
Great video, that engine has far fewer points than I would have imagined! However, the cowling it sits in looks very firmly anchored to the body of the plane, which is more like the Star Trek equivalent of the nacelle and pylon, whereas the A10 engine in the vid is more akin to the warp coils.And I say, apply 60 years of jet engine mounting knowledge to the warp engines, which are supposed to mimic "quick change units". While I acknowledge the question of scale, jet engines use surprisingly few mount points to stay attached to planes and require none of the overbuilt internal support too often proposed for warp nacelles.
Here's a short video on the installation of an A-10 Warthog engine. (4:44 long. Relevant view at about 0:32.)
Exactly what I was going to say. Very similar to a car engine. I have an mid 70's chevy and the engine/transmission is held in place with 3 bolts. I know from my hobby of studying aircraft accidents that how the engine is bolted on is one of the most highly inspected parts of a plane. But in terms of structue, the warp pylons would be more like the wings. They are long and thin and have to endure a lot of stress. So the pylons and their attachment at either end would need to be very strong. It either needs to be very flexible to avoid breaking, or be stiff enough to endure the necessary forces. Wings have come in both types.Great video, that engine has far fewer points than I would have imagined! However, the cowling it sits in looks very firmly anchored to the body of the plane, which is more like the Star Trek equivalent of the nacelle and pylon, whereas the A10 engine in the vid is more akin to the warp coils.
Ah, I completely take your point there! It was an interesting study in 20th century style engineering (and one I followed with interest back in the day) but then he went and broke his own rules by introducing a "super strong plate" at the top of the dorsal section. This mechanism (made of unspecified materials) would both attach the dorsal to the saucer securely at all times AND allow for saucer separation when required.Anyway, what I am really arguing against is the stupid over-the-top BS like Cary L Brown posted in his take on the Enterprise back in the day.
https://www.trekbbs.com/threads/another-take-on-the-original-enterprise.89810/page-3#post-2886453
https://www.trekbbs.com/threads/another-take-on-the-original-enterprise.89810/page-13#post-3030095
This post, however has an image that is topical.
https://www.trekbbs.com/threads/another-take-on-the-original-enterprise.89810/page-6#post-2917560
*(mostly)
We use essential cookies to make this site work, and optional cookies to enhance your experience.