Relax wrote:Yes, tonnage for SDP must vastly increase.
**Note regarding your post: MK-16 SDP will never happen. Range. May even go to 4 stage MDM instead of 3 in the near future.**
I think that'd depend on the effective range of Keyhole II Apollo FTL control.
The (4-stage) system defense missiles have the advantage of fighting on prepared ground, where the system will have been seeded with Mycroft FTL fire-control relay nodes -- making the inherent range limits of any single Apollo link fairly irrelevant.
Ships can't count on that same advantage. We don't have a solid number on the max useable range of Apollo - just two [edit: 3; thanks Kytheros] widely different data points.
* 2.97 lm (53,400,000 km) is within range [AAC:Ch57]
* 4.56 km (82,000,000 km) is within range [StfS:Ch13]
* 8.34 lm (150,000,000 km) is beyond effective range [AAC:CH68]
(65,726,640 km is max continuously powered range of a Mk23)
So adding range may, or may not, be useful to them; and in my opinion they'd only add the drive if it added useful (controllable) extra range. [Ok, Kytheros's info shows that there is usable Apollo range beyond max powered Mk23 range]
I'm just not sure what RFC/Bunine have the the max continuously powered range of a 4-drive MDM calculated as.
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Relativity tangent:
You can't calculated it the same way that the existing missiles seem to be done (ignoring the effects relativity) -- if you did the calculations would show terminal velocities greater than c. (oops)
Without relativity a Mk23, accelerating at 42000g for 540 seconds reaches:
65.7 million km range, at 0.81c terminal velocity
(agrees with the books)But, if I did it correctly, throwing in relativity those numbers drop to:
57.4 million km range, at 0.63c terminal velocity
But how to reconcile a 3-drive missile, calculated w/o relativity, to a 4-drive missile that can't completely ignore it isn't exactly obvious.