Would this be a new launch-booster or the modification of an existing in production design?
 
Would this be a new launch-booster or the modification of an existing in production design?

It wouldn't be Aster as the 15's booster is 1.6m long, or VL-SeaWolfs. Presumably it would be a new design.

The papers authors were from Bayern Chemie and MBDA. Presumably they chose that total length (roughly 4.8m for Missile and Booster) for a specific application. Germany was looking at MEADS at the time, but the interceptor was the PAC-3 MSE (along with IRIS-T SL). Were they studying Meteor as a potential missile alongside PAC-3? But PAC-3 wis 5.2-5.3m long, so why would they not use that additional space for a longer booster? Or is m.1.6 the ideal speed for handover to the integral booster to get it to m2.5 and ramjet function?
 
It wouldn't be Aster as the 15's booster is 1.6m long, or VL-SeaWolfs. Presumably it would be a new design.

The papers authors were from Bayern Chemie and MBDA. Presumably they chose that total length (roughly 4.8m for Missile and Booster) for a specific application. Germany was looking at MEADS at the time, but the interceptor was the PAC-3 MSE (along with IRIS-T SL). Were they studying Meteor as a potential missile alongside PAC-3? But PAC-3 wis 5.2-5.3m long, so why would they not use that additional space for a longer booster? Or is m.1.6 the ideal speed for handover to the integral booster to get it to m2.5 and ramjet function?

I'm pretty sure Meteor was proposed as a low-cost interceptor for MEADS. (Working from memory, but I posted that idea years ago)

Post in thread 'Medium Extended Air Defense System (MEADS)' https://www.secretprojects.co.uk/threads/medium-extended-air-defense-system-meads.17821/post-182303
 
The papers authors were from Bayern Chemie and MBDA. Presumably they chose that total length (roughly 4.8m for Missile and Booster) for a specific application. Germany was looking at MEADS at the time, but the interceptor was the PAC-3 MSE (along with IRIS-T SL). Were they studying Meteor as a potential missile alongside PAC-3? But PAC-3 wis 5.2-5.3m long, so why would they not use that additional space for a longer booster? Or is m.1.6 the ideal speed for handover to the integral booster to get it to m2.5 and ramjet function?
I suspect that M=1.6 was the ideal speed for handover.

I mean, we know that the integral booster is intended to get Meteor from aircraft speed to ramjet speed, so it's probably got a ~300knot minimum speed.
 
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