Did not know if these had been posted here on SD...but here's an excellent sequence of four photos showing the cold launch of a VLS HQ9 from the PLAN's 170 Lanzhou
Type 052C:
Nice pictures.
Jeff, could you explain to me the differences btween cold and hot lunches?
What are the pros and cons?
Thank you.
not trying to be Jeff but hot launches are a lot more efficient because the rocket uses it own internal propulsion as oppose to a cold launch where the ship has to "help" in launching the missiles thus using it's own separate internal launch system. It is thus heavier and takes up additional space compared to hot launch systems.Did not know if these had been posted here on SD...but here's an excellent sequence of four photos showing the cold launch of a VLS HQ9 from the PLAN's 170 Lanzhou
Type 052C:
Nice pictures.
Jeff, could you explain to me the differences btween cold and hot lunches?
What are the pros and cons?
Thank you.
sub surface missile launch uses cold launch for obvious reasons at least until someone can efficiently invents a singular propulsion system that can propel a missile in both liquid and air!
Uh, no?sub surface missile launch uses cold launch for obvious reasons at least until someone can efficiently invents a singular propulsion system that can propel a missile in both liquid and air!
No. Rockets don't need air, that's why they are called "rockets".Solid propellant means they need oxygen to be present in the environment in which they are ignited.
I'd hate to have cryogenic fueled missiles on board my submarine.I think if you have liquid fuel based engine (like hydrogen/oxygen) it is possible to propel the missile in water.
Solid propellant engine is preferred for military ballistic missile because it provides larger thrust, does not need to be fuelled before launch, and also don't have a short expiration date (as the case with say hydrogen peroxide)
Solid propellant means they need oxygen to be present in the environment in which they are ignited.