Excerpt from "USAF Advanced ICBM Concepts (U)" (1965) (Ref. 24)
[...]
The TITAN II improvement proposal includes several MIRV configurations:
1. 6 x MARK-17 reentry vehicles
2. Two buses each carrying 8 x MARK 12 [DELETED] RV
3. Five buses each with 6 x MARK 100 [DELETED] advanced technology reentry vehicles.
Technical Details of the W67/Mark 17
Normally they are very cagy about reentry vehicle and RV warhead weights, so I was surprised to come across them.
The total RV and warhead weight was planned to be 410 kg (900 lb) and by November 1966 they had managed to get it down to 425 kg (938 lb). The bare warhead weight was 306 kg (675 lb).[5, p. 43] The yield is classified, but it was comparable to that of the W56/Mark 11, i.e. 1.2 Mt.
Did SAC ever considered procuring more than 54 operational Titan II ? was there a higher number early on, say in 1960-61 ?
Did SAC ever considered procuring more than 54 operational Titan II ? was there a higher number early on, say in 1960-61 ?
c. Titan II (Advanced). A highly-reliable, storable liquid propellant missile capable of carrying a payload of 12,000 lbs. at least 5,500 nm with a CEP of [REDACTED]. Re-entry body capable of carrying highly-sophisticated penetration aids. [REDACTED SENTENCE] Hardened to 500 psi. Employed primarily against very hard nuclear storage sites and ABM defenses. Some retained in Reserve for very hard targets. Required availability 1968.
The rationale for the Advanced Titan II system depends on the requirement for a very high yield weapon [REDACTED SENTENCE] Based on military considerations, the need for this system is not apparent. The Hickey Study indicates that Titan II would be able to deliver a [REDACTED SENTENCE] and is competitive with the advanced version.
Titan II
The 18 extra Titan missiles proposed by the Air Force would cost approximately $372 million to procure and operate for 5 years. The Titan II has a substantially larger payload than Minuteman. It will be able to deliver 9 megatons rather than 1.2 megaton warheads now programmed for Minuteman. But the total system cost of a Titan II is about four times that of a Minuteman hard and dispersed. At equal cost, four Minutemen are to be preferred to one Titan because, first, they are less vulnerable, and second, they provide more target coverage.
Moreover, we already plan to have a substantial force of Atlas and Titan which should be adequate for those special purposes requiring large payloads. Therefore I do not recommend procurement of additional Titans.
Where do I find the document?W. Emrick and M. Watter, USAF Advanced ICBM Concepts, PEN-X Paper 58, Institute for Defense Analyses, (1965) (Title U, Report SRD)
Mk 12 is MM3 RV of 170 KT.
Mk 100 is ???
Mark 17 is...
https://super-octopus.com/2022/08/13/some-details-on-the-w67-mark-17/
W. Emrick and M. Watter, USAF Advanced ICBM Concepts, PEN-X Paper 58, Institute for Defense Analyses, (1965) (Title U, Report SRD)
Mk 12 is MM3 RV of 170 KT.
Mk 100 is ???
Mark 17 is...
https://super-octopus.com/2022/08/13/some-details-on-the-w67-mark-17/Technical Details of the W67/Mark 17
Normally they are very cagy about reentry vehicle and RV warhead weights, so I was surprised to come across them.
The total RV and warhead weight was planned to be 410 kg (900 lb) and by November 1966 they had managed to get it down to 425 kg (938 lb). The bare warhead weight was 306 kg (675 lb).[5, p. 43] The yield is classified, but it was comparable to that of the W56/Mark 11, i.e. 1.2 Mt.
Blog author here.So the Mk-17 RV was a sphere-cone type RV like the Mk-12?
I actually stumbled across a document a while back that had the precise yield of the Mk17/W67, which turned out to be 1500 kt.
https://nsarchive.gwu.edu/document/...-deputy-assistant-secretary-politico-military (see page 14)
I actually stumbled across a document a while back that had the precise yield of the Mk17/W67, which turned out to be 1500 kt.
https://nsarchive.gwu.edu/document/...-deputy-assistant-secretary-politico-military (see page 14)
There's a 1800 kiloton figure out there too, I think in one of the USAF Ballistic Missile Programs histories.Excellent find. That's on the low end of what I had estimated, but I can't argue with the actual numbers in front of me.
Do you know which one? To the best of my knowledge I have read every one of those that has been released, and I don't recall seeing a yield figure for the Mark-12(H)/Mk17/W67 in any of them, let alone a 1800 kt figure.There's a 1800 kiloton figure out there too, I think in one of the USAF Ballistic Missile Programs histories.
I just re-OCR'ed the 1964 to 1970 copies and did some keyword searches. No dice.Do you know which one? To the best of my knowledge I have read every one of those that has been released, and I don't recall seeing a yield figure for the Mark-12(H)/Mk17/W67 in any of them, let alone a 1800 kt figure.
Ah, here it is:Do you know which one? To the best of my knowledge I have read every one of those that has been released, and I don't recall seeing a yield figure for the Mark-12(H)/Mk17/W67 in any of them, let alone a 1800 kt figure.
Standart Titan II had payload of 8,200 lb for 9 MT warheadTitan II Advanced -- 12,000 lb payload to 5,500 nm.mi; with yields around (or over) 50 MT.
Depends how hard the targets are. If you're imagining the enemy having something like DUCC, then multiple 50 Mt weapons are needed to kill it.Now to use larger yields up to 50 MT against hardened targets is total overkill
Intrigued by the “Improved Capability Minuteman” reference, which looks to be on the low end of the WS-120 range.Ah, here it is:
https://web.archive.org/web/2020022.../DOD/Project_List_CY1964_IIIb_SEP-15-1964.htm
Not one of the official histories at all, but a 1964 memo for SecDef. Probably a preliminary figure, given the earlier date, and a heavier warhead than the later version, but perhaps an indication of what was hoped for.
It does seem to be the early stages of that effort.Intrigued by the “Improved Capability Minuteman” reference, which looks to be on the low end of the WS-120 range.
It'd take a heck of a lot of megatons to blast out Cheyenne Mountain et sim for sure!Depends how hard the targets are. If you're imagining the enemy having something like DUCC, then multiple 50 Mt weapons are needed to kill it.
Very interesting.Ah, here it is:
https://web.archive.org/web/2020022.../DOD/Project_List_CY1964_IIIb_SEP-15-1964.htm
Not one of the official histories at all, but a 1964 memo for SecDef. Probably a preliminary figure, given the earlier date, and a heavier warhead than the later version, but perhaps an indication of what was hoped for.
I also can't help but wonder if there's something similar going on with both warheads, and that someone has their thumb on the scale. If you wanted Polaris to look better than Minuteman, you might well report the 'good day, fresh tritium' yield for the former and the 'bad day, end of life' for the latter.My impression was that Livermore promised that the W62 warhead would be 200 kt and then fell short. For them to state it's 170 kt in 1964, years before first production unit is surprising.
The W58 is also interesting. Most sources I have seen were very confident in a 200 kt yield. 225 kt is the yield often quoted for the British Chevaline warhead though, which is supposed to be a the same secondary in a new reentry vehicle and using a new rad hard primary.
I have to wonder if the 200 vs 225 kt yield figure has to do with limited life components. Maybe it gets 225 kt with new boost gas, and 200 kt at end of life? It might also be some confidence factor, something like average yield is 225 kt, and a random W58 warhead as a 99% chance of producing at least 200 kt?
Perhaps, but the author is Harold Brown, who at the time was director of Livermore. With both warheads being Livermore designs, this seems unlikely.I also can't help but wonder if there's something similar going on with both warheads, and that someone has their thumb on the scale. If you wanted Polaris to look better than Minuteman, you might well report the 'good day, fresh tritium' yield for the former and the 'bad day, end of life' for the latter.
He was DDRE from 1961-65 and SecAF from 1965-69. The context of the memo is a briefing for McNamara on whether next-gen missiles were needed to survive a Soviet MIRVed first strike. I think the warhead discussion is adjacent to that.Perhaps, but the author is Harold Brown, who at the time was director of Livermore. With both warheads being Livermore designs, this seems unlikely.
Ah, you are right. I didn't realise he only lasted a year as director.He was DDRE from 1961-65 and SecAF from 1965-69. The context of the memo is a briefing for McNamara on whether next-gen missiles were needed to survive a Soviet MIRVed first strike. I think the warhead discussion is adjacent to that.