Ta 154 A
of the regular cockpit the TA 154A should get a stripped down version,
which would have been connected to the fuselage by four bolts, just
of the 5. bulkhead and only would be used for flyover. At operation
the cockpit would have been exchanged with a hollow charge warhead. Any
technical equipment not necessary was canceled.
warhead would have been a hollow charge of 2500kg, 3000kg or max.
weight. Depending on the weight it would have been mounted in more or
distance to the bulkhead. When useing the 3500kg charge additional
of 100kg would be mounted to the rear, to even the centre of gravity.
front landinggear would have been connected to the warhead with struts
that seperate by explosive bolts.
main landingear wouldn't be changed at all except for increasing the
on the shock absorbers from 60 to 97 atü (athmospheres). Starting
the Mistel would been possible in this configuration from an concrete
but landing never was an option.
guidance aircraft would have been the FW190 A8. Which would be mounted
atop the Ta 154 by a scaffold. All controls of the Ta 154 would be
by the FW190 A8. During approach run both aircraft would be fueled by
Ta 154 . This would increase the range immensely.
from the Ta 154 was planned to be managed by explosive bolts. Therefore
the rear strut was blown first to ensure a safe seperation.
run would been accomplished by the Fw 190 A8 and final approach by
controlles called "Lagekommando für Höhensteuerung". As a
control a TSA1 was intended.