There really is no difference to the rockets themselves, they are all varying forms of pointy metal pipes filled with boom powder. The only difference is the payload they carry; whether they are humans or spaceborne vessels like satellites, or explosives of various descriptions with which to destroy and kill.
If you disagree, and you've certainly made it clear you do, you can put forth counterarguments instead of claiming quackery.
One quick question though, what was the "powder" used on, say, the Apollo missions?
I've always heard the Saturn V launch had a J-2 liquid propellant rocket engine that used used liquid oxygen and liquid hydrogen.
The Saturn V used RP-1 and liquid oxygen for the first stage, and liquid hydrogen and liquid oxygen for the second and third stages. The Apollo CSM used dinitrogen tetroxide and "Aerozine 50", a 50:50 mix of hydrazine and UDMH hypergolic fuels that was originally used for the Titan II ICBM.
Further reading:
https://en.wikipedia.org/wiki/Saturn_V
https://en.wikipedia.org/wiki/Apollo_command_and_service_mod...
Relatively slow controlled energy release for thrust isn't particularly evoked by the word BOOM!!
Otherwise simplifying rockets and missiles as they are today to tubes of slow release thrust (with some additional wrinkles such as side thrust | directional thrust to 'balance' load over thrust, multi stages, etc) seems innocent enough.