SamuraiBlue
Captain
Re: JMSDF Akizuki Class DDG (19DD AEGIS-like)
Sorry I never intend to imply that DRE AAM-4 will have similar range of SM-6 which I believe is somewhere around 350Km but the normal version has a range of 100Km.
Before we go further I believe that we need to understand the difference between conventional solid rocket propellent and the propellent for Ducted Rocket Engine.
Solid rocket propellent consists of two components, an accelerant(fuel) and oxidizer in which the two chemically react as combustion to gain thrust. On the other hand, Ducted Rocket Engine propellent consists of only an accelerant in which is heated to evaporate the solid propellant and then mixed with air in another chamber where it is combusted to gain thrust.
The greatest gain of this technology is that theoretically it carries twice the amount of energy compared to conventional solid rocket since it does not carry any oxidizer.
This is purely speculation but I believe that the DRE AAM-4 would have a range somewhere around 200Km and a ship launched missile will have similar range equipped with a small initial booster stage similar to a cruise missile.
Interesting -- is the intention to produce a surface launched missile based off AAM-4 that can achieve SM-6 ranges, or an air launched AAM based off AAM-4?
I find it very difficult to imagine an AMRAAM sized missile having a slant range of over 200km. Flipside, is that if an AMRAAM sized missile can achieve that kind of range eventually, then an SM-6 sized missile could theoretically be able to achieve many times that (whether they have the electronics to engage such a target is another matter of course).
Sorry I never intend to imply that DRE AAM-4 will have similar range of SM-6 which I believe is somewhere around 350Km but the normal version has a range of 100Km.
Before we go further I believe that we need to understand the difference between conventional solid rocket propellent and the propellent for Ducted Rocket Engine.
Solid rocket propellent consists of two components, an accelerant(fuel) and oxidizer in which the two chemically react as combustion to gain thrust. On the other hand, Ducted Rocket Engine propellent consists of only an accelerant in which is heated to evaporate the solid propellant and then mixed with air in another chamber where it is combusted to gain thrust.
The greatest gain of this technology is that theoretically it carries twice the amount of energy compared to conventional solid rocket since it does not carry any oxidizer.
This is purely speculation but I believe that the DRE AAM-4 would have a range somewhere around 200Km and a ship launched missile will have similar range equipped with a small initial booster stage similar to a cruise missile.