The Katyushas were invented by the Soviets and used in WW2. They were trucks with rails firing a bunch of small rockets with a range of 3 to 12 km.
These were solid-fuel rockets, but I would like to know what exact rocket fuel they used, because it relates to a few of my other questions:
Why was the V2 not a solid rocket?
What was the first rocket to use solid APCP fuel?
Edit: Forgot to post my research. So far the closest thing I found was this page from Russianspaceweb.com on the RT-1, apparently Russia's first large solid rocket. It says "These engines burned essentially same powder fuel which had propelled the famous 1930s-vintage Katyusha rockets. (177)" and down in the chart it says "Propellant Solid --- RSD-4K". I tried googling that but got nothing.
therefore, OG Filippov and SA Serikovs developed a fundamentally new gun-cotton-TNT powder (TAP) containing 76.5% of gun-cotton, 23% TNT and 0.5% tsentralita.
Not sure what "tsentralita" means, but gun-cotton is nitrocellulose. $\endgroup$