Editing R4M (section)

== Technical specifications (R4M) ==
[[File:R-4M_Orkan_(3D-iso).jpg|borderless|600px|right]]
;General
*'''Name''' − Rakete, 4 kilogramm, Minenkopf (R4M)
*'''Type''' − Folding-fin, [[Air-to-air rocket]]<ref name="ABC" />
*'''Total length''' − {{convert|812|mm|in|abbr=on|sigfig=3}}<ref name="ABC" />
*'''Total weight''' − {{convert|3.85|kg|lb|abbr=on|sigfig=3}}<ref name="ABC" />

;Warhead
*'''Type''' − [[High-Explosive, High-Capacity]]<ref name="ABC" />
*'''Caliber''' − {{Convert|55|mm|in|abbr=on|sigfig=3}}<ref name="ABC" />
*'''Length''' − {{convert|200|mm|in|abbr=on|sigfig=3}}<ref name="ABC" />
*'''Wall thickness''' − {{convert|0.8|mm|in|abbr=on|sigfig=3}}<ref name="ABC" />
*'''Explosive Charge''' − {{convert|520|g|lb|abbr=on|sigfig=3}} ''HTA 41''{{efn|name=HTA}}<ref name="ABC" /> ([[torpex]])
*'''[[Fuze]] model''' − ''AzR2'' nose fuze<ref name="ABC" />
*'''Fuze length''' − {{convert|65|mm|in|abbr=on|sigfig=3}} (total), {{convert|15|mm|in|abbr=on|sigfig=3}} (internal)<ref name="ABC" />

;Rocket engine
*'''Diameter''' − {{convert|55|mm|in|abbr=on|sigfig=3}} (engine)<ref name="ABC" />
*'''Length''' − {{convert|410|mm|in|abbr=on|sigfig=3}} (engine), {{convert|148|mm|in|abbr=on|sigfig=3}} (tail section)<ref name="ABC" />
*'''Fin-span''' − {{convert|242|mm|in|abbr=on|sigfig=3}}<ref name="ABC" />
*'''Fin-swivel''' − 100°<ref name="ABC" />
*'''Propellant type''' − Solid fuel [[diethylene glycol]] tube<ref name="ABC" />
*'''Propellant dimensions''' − {{convert|340|mm|in|abbr=on|sigfig=3}} (length), {{convert|12|mm|in|abbr=on|sigfig=3}} (internal diameter), {{convert|45|mm|in|abbr=on|sigfig=3}} (external diameter)<ref name="ABC" />
*'''Propellant weight''' − {{convert|0.815|kg|lb|abbr=on|sigfig=3}}<ref name="ABC" />
*'''Combustion chamber''' − {{convert|2.5|mm|in|abbr=on|sigfig=3}} thick venturi-pipe ending with a [[nozzle]]<ref name="ABC" />
*'''Nozzle dimensions''' − {{convert|110|mm|in|abbr=on|sigfig=3}} (length), ({{convert|13|mm|in|abbr=on|sigfig=3}} (internal top diameter), {{convert|45|mm|in|abbr=on|sigfig=3}} (internal base diameter)<ref name="ABC" />

;Performance
*'''Max thrust''' − {{convert|245|kp|lbf|abbr=on|sigfig=3}}<ref name="ABC" />
*'''Burn time''' − 0.75 s<ref name="ABC" />
*'''Velocity''' − {{convert|525|m/s|ft/s|abbr=on|sigfig=3}} (initial), {{convert|125|m/s|ft/s|abbr=on|sigfig=3}} (at {{convert|1000|m|yd|abbr=on|sigfig=3}})<ref name="ABC" />
*'''Range''' − {{convert|1500|m|yd|abbr=on|sigfig=3}} (max),<ref name="ABC" /> {{convert|600-1000|m|yd|abbr=on|sigfig=3}} (effective)