VERSIONS – J21 prototype, J21A-1/A-2/J(A)21A-3, J(A)21RA/RB
Revised nose profile/
nose gear cover
Revised, squarer
fin shape
1 x 13.2 mm (.52 in) m/39
machine gun with 310
rounds per gun in each
tail boom
2 x 13.2 mm (.52 in) m/39 machine
guns with 325 rounds per gun,
1 x 20 mm (.79 in) Bofors m/41A
cannon with 130 rounds
Provision for centreline ventral gunpack
400 lt (88 Imp gal, 106 US gal)
wingtip tanks
J(A)21RA – with RM1 (de Havilland
Goblin 2) centrifugal flow jet engine;
J(A)21RB – with RM1A (de Havilland
Goblin 3) centrifugal flow jet engine
Jet-powered version, details as J21
prototype unless otherwise indicated
New rear engine section to accommodate Goblin engine
Tailplane raised above jet efflux
New, larger intakes
Radiators deleted, replaced by additional fuel tanks
Strengthened tail structure
Revised, rounded windshield and canopy
Wing gunport fairing
K-14 automatic gun sight
Pitot moved
to port wing
Wing flaps, no centre
fuselage flap
Bulbous engine fairing
Revised elevator
with single trim tab
Exhaust
Main undercarriage units moved
further forward by 200 mm
(7.87 in), up by 300 mm (11.8 in)
and angled forwards
Airbrakes above
and below wing
Revised cockpit layout/
instruments
New hydraulic pump and
pressurised air system
Leading edge
extended forward
J(A)21RA/RB
Revised nose profile/
nose gear cover
Revised, squarer
fin shape
1 x 13.2 mm (.52 in) m/39
machine gun with 310
rounds per gun in each
tail boom
2 x 13.2 mm (.52 in) m/39 machine
guns with 325 rounds per gun, 1 x
20 mm (.79 in) Hispano-Suiza m/41A
cannon with 130 rounds
Gun camera
400 lt (88 Imp gal, 106 US gal)
wingtip tanks ((A)21A-3)
J21A-1 (shown);
J21A-2 – revised centre under
fuselage flap, armament all
produced by Bofors (1 x 20 mm
(.79 in) Bofors m/45 cannon
with 130 rounds);
J(A)21A-3 – attack version
with hardpoints on centreline
and under outer wings for
rockets and bombs, also
wingtip tanks (shown)
Production version, details as J21
prototype unless otherwise indicated
Wing gunport fairing
K-14 automatic gun sight
(J21A-2/A-3)
Centre under fuselage flap
split into three sections at rear
Pitot moved
to port wing
J21A-1/A-2/J(A)21A-3
Tail boom incorporating main landing gear unit
Tricycle undercarriage nose gear
unit in lower forward wheel well
SAAB Mk.1 ejector seat
Three-bladed pusher propeller
faired into streamlined fuselage
Rounded fin with
large rudder
Exhaust stacks (port/starboard)
Starboard side intake
Bulged side canopy panels
Inner wing root radiators
with ground cooling fans
disengaging in flight
Landing light in nose of each boom
Radio antenna on
starboard boom
Retractable boarding ladder on lower starboard side
Swept outer section to wing
Pitot on starboard wing
Wing gunports blanked off
Upper canopy section hinged
and opening to port
No nose armament
SFA licence-built Daimler Benz
DB 605B inline engine
Hydraulically
powered ailerons
Twin boom/tailplane
assembly with single,
large elevator with
trim tabs
VDM constant-speed
fully-feathering
propeller
3 x hydraulically operated flaps
(1 x each wing outer section,
1 x under centre wing section
J21 prototype
21001
J21: 3
ILLUSTRATIONS: © ADRIAN DAVID MOORE 2015 • NO ITEMS MAY BE REPRODUCED WITHOUT THE PERMISSION OF THE COPYRIGHT HOLDER
ILLUSTRATIONS: © ADRIAN DAVID MOORE 2015