468192

THIS PAGE DECLASSIFIED IAW EQ 129 8
,
- e -
APP : 1ivDI X I X
c a r r y i n 5 o f' a d d i t i ou a l f u e l . ri l l r es u l t i r . a iur or Shl f t i ng o f
the center of ravitf .
iaxe-oif Distance : 4 , 000 f eet , r equired ler: th of runway a b out
+ ,
o C f e e t by a rri a t h e o f ZUO f e et .
Av er a ;; e s pe e ci e n r ou t e : 3 b o u t 2 4 0 -
c 5 0 ni l e s p er h our .
aximum speed : about 280 - 300 miles per hour .
Decisions have to be made wheth er
. a .
A modification for an additior . al fuel tank should be carr i ed ou t;
b .
Ca l cu l ations regarding a radius of action of 90 7 rniles should
ne
undertak en .
I a a de c i s i on r eg ar di ng poi n t a .
i s ma de i mr g e di a t e l y ,
t h er e wi l l
proba bl y be nc; delay in
flying the mission.
2 .
Navibational Matters ( geared to low- l evel fligh t)
a . B u ilt i n : Three- di ©assiona l con trol in the Junkers 88 and
'
radio set 16 Z in tb e Bayrir,che Flugzeigwerke 109 .
on
R esulting Capability : Very precise course- fl ying and approach
with radio set 16 Z toward radio buoy
"Swan
(Range 50 -
60 mil es at a fli ht
altitude of 660 f ee t) .
b .
Addition
of lon -wave receiver set Radione so that the sun 's
position can be f ully utilized ,
for instance at Stavanger an d
Ma r s e i .
l l e .
c .
Th e most advanta ;eous solution seems a combination of both
systemsFor the return flight one can either
use emeroency DF
ao z ṛ i[ approach
flioht toward the sun or radio set 16 Z for
comrnunication with a ground sta tion transmitter 16 .
THIS PAGE DECLASSIFIED IAW EQ 129 8