one of my biggest questions about these standard missiles is regarding the mass of the mk-72 booster, i had seen that brochure you sent before and i didn’t understand why the mass was so low at 680kg, when i made my attempt on modelling the SM-2 BLK IV i assumed the booster mass was 740kg, and the entire stack 1496kg, i got these estimates from this brochure, it has the values of 705.7kg for the SM-2 MR (upper stage only) and the SM-2 AEGIS ER has a mass of 1451kg (1451kg - 705kg = ~746kg), so thats where i got the mass value of 746kg for the mk-72, the SM-2 BLK IVA has an extra 45.3kg of weight compared to the SM-2 ER, and the blk IV was what i was aiming for so i added that extra weight to the upper stage, i know the SM-6 is heavier than these missiles but there’s more info around for the SM-2 family, this navy website has some small inconsistencies with the weight on that brochure, which is annoying
i assumed 467kg of fuel at around 268 ISP for the booster (kinda optimistic imo), i’ll explain why that isp is so high inside the SM-3 section, i have no idea how accurate most of this attempt is
i modelled the first stage around known boost/sustainer burn times and thrust ratios for the RIM-66B, the burn time i used this video, it shows the upper stage burning for at least 34 seconds and at most 38 seconds(i used a total burn time of 36.2s), all that together the claimed top speed of mach 3.5 and max range of 166km for the upper stage, the CxK value i used was 1.25, it was based off the RIM-24 gaijin modelled and added to the game, that has a CxK of 1.4, at first i tried to keep the same value but i couldn’t achieve some criterias without very high ISPs so i decided to lower the drag a little bit.
my final goal for the full stack was to achieve a speed of at least mach 6 in a normal flight (not going 90° up), that number comes from this document
Spoiler

source: Recent Events in Guidance, Navigation and Control by Michael Polites, Darin Groll, and Johnny Evers

some more brochures and general info i found about the standard missile family
SM-2/3
i unfortunately found a document stating the mass of the third stage motor used in the SM-3 only and another convenient document stating the entire mass of the SM-3 stack, so i was left with a mass value for the rest of the missile that is shared with the SM-2/6

AEGIS LEAP Intercept (ALI)/STANDARD Missile Three (SM-3)
this states the fuel mass for the third stage is is ~93kg
this other document was my source for the entire fuel mass of the SM-3 stack

Hazard Assessment Testing of the SM-3 Block IA Missile
that would leave the MK-72 + MK-104 stack with 841kg of propellant, the upper stage alone was getting too fast on it’s own and the full stack wasn’t getting to mach 6, so i didn’t know what to do to make this balance better and achieve both goals, the 1st stage ended up with an ISP too high, and has you could see despite getting optimistic values for both stages i still couldn’t get the mach 6 objective
more brochures and documents
HIGH PERFORMANCE BOOST PROPULSION FOR THE NAVY THEATER MISSILE DEFENSE - this one talks about what would become the 21 inches 2nd stage for the SM-3 BLK II, but it still has some good general info
source for the images: 5th Grade Career Activity Lesson

