Wait, did they make a hot launch version?!
That looks like a 2 canister hot launched missile, don't think I've seen that before.
Wait, did they make a hot launch version?!
That looks like a 2 canister hot launched missile, don't think I've seen that before.
True see @1:04 of S-300 ejection stage, it's probably what photo captured....it is just a part of the ejection mechanism where the photo was taken "early" in the ejection cycle making it seem like it is fire from the missile's exhaust, but when it is actually just from the ejection system instead.
Interesting, so Chinese cold launch VLS uses some form of combustible material, whereas Russian S300 and others use compressed gas?
Interesting, so Chinese cold launch VLS uses some form of combustible material, whereas Russian S300 and others use compressed gas?
Hard to say... I think the "combustion" artefact we see in the HQ-9 and HQ-16 photos happens in the early stage of the cold launch ejection and happens so quickly that you really need the photo taken at just the right time to capture it.
Normal video doesn't seem fast enough to capture it either, looking at a few launch videos online.
For S-300 I wouldn't be surprised if they also have the combustion artefact but none of the photos online happen to capture it at that exact moment. (Or maybe they do but I have yet to find one).
Hard to say... I think the "combustion" artefact we see in the HQ-9 and HQ-16 photos happens in the early stage of the cold launch ejection and happens so quickly that you really need the photo taken at just the right time to capture it.
Normal video doesn't seem fast enough to capture it either, looking at a few launch videos online.
For S-300 I wouldn't be surprised if they also have the combustion artefact but none of the photos online happen to capture it at that exact moment. (Or maybe they do but I have yet to find one).
True see @1:04 of S-300 ejection stage, it's probably what photo captured.
Like the S-300P series systems, the S-300V uses the cold launch technique, originally developed for rapid reload ICBM silos, ejecting the missile before its motor is fired. These 9M83 SAMs are being launched from a 9A83 TELAR, which uses its elevated directional antenna to provide the 9M83 with both midcourse command updates and terminal phase high power continuous wave illumination of the target. Antey claim the semi-active seeker will acquire a 0.05 square metre RCS target at 16 nautical miles (Rosvooruzheniye).