Mk.1 to Mk.9
            pre-Mk. 1
            Mk. 1
            Mk. 2
            Mk. 3
            Mk. 4
            Mk. 5
            Mk. 6
            Mk. 7
            Mk. 8
            Mk. 9
      Mk.10
      Mk.11
      Mk.12
      Mk.14
      Mk.15
      Mk.16 high-speed
      Mk.16 low-speed
      RetroFit / Upgrades

Overview

After some 23 years of development, the design of the Martin-Baker Ejection Seats was becoming somewhat complex, and towards the end of the 1960 decade a new design was put in hand which eventually became the Mark 9 seats. The general design features of the ejection gun and guide rail, the barostatic time-release unit, the drogue gun and the personal equipment connector were retained, but considerable changes were made to the general seat structure, the drogue container, the parachute and the seat pan. These design changes resulted in a marked improvement in the appearance of the seat and in personal comfort for the occupant. These seats were equipped with power retraction and a completely new gas-operated seat firing system, superseding firing cables and utilising one firing handle only, mounted on the seat pan, the face screen and its firing cable being dispensed with.

 Specifications

Specifications
Mk 9 (Jaguar)
 
 
Operating ceiling
50 000+ft (15,250 m)
Minimum height/speed
Zero/zero
Crew boarding mass range
9B Mk 1, Mk 2 and Mk 3 - 73.0 to 112.0 kg
 
9B Mk 4 - 65.0 to 135.0 kg
Crew size range
3rd to 98th percentile. As defined in Survey of 2000
 
Royal Air Force Aircrew 1970/1971
Maximum Speed for ejection
600+ KIAS
Parachute type
Irvin IAC 1 24 B/10704
Parachute deployment
Drogue assisted
Drogue parachute type
Duplex drogues, 22 in. and 5 ft
Drogue deployment
Drogue gun. Cartridge generated gas. Initiated
 
by 0.55 sec clockwork time-delay, tripped by trip rod
Harness type
Combined, skeletal torso harness with rip cord
Ejection seat operation type
Ejection gun and multi-tube rocket pack
Ejection gun
One primary cartridge, two secondary
 
cartridges, 72.75 in. stroke, 64 ft/sec
Ejection initiation
Handle on seat pan initiates gas operated seat
 
firing system
Electronic Sequencer
No
Barostatic time-release unit
Yes, with 2 sec delay to give time for speed
 
to decrease. Trip rod initiated
Automatic back-up unit
No
Manual override handle
Yes
Guillotine
Yes, early variant
Timers
Time-release for canopy jettison
Seat adjustment
Up/down, actuator operated, 115 V ac motor
 
Pitch control for rocket motor adjustment to
 
allow for varying weights of occupant
Arm restraints
No
Leg restraints
Yes, two garters
Oxygen supply
Bottled oxygen
Personal survival pack
Yes with liferaft (option)
Aircrew services
Intertechnique controller with oxygen flow
 
sensor and pressure warning
 
Personal equipment connector (PEC) provides
 
connections for
 
- main oxygen
 
- emergency oxygen
 
- anti-g suit
 
- mic/tel
Command ejection
No
Canopy jettison
Yes, also drogue container is shaped and
 
strengthened to effect canopy penetration if necessary
Miniature detonating cord
No

 How it works

Seat firing handle pulled
Harness retraction operated
Canopy jettison initiated
Ejection gun fires, seat moves up guide rails, secondary cartridges fire
Leg restraint cords tighten until the rivets shear
As seat rises, static line initiates drogue gun time-delay
As seat rises, static line initiates barostatic time-release unit
Aircrew services and electrical lead disconnected
Emergency oxygen turned on
Underseat rocket pack initiated
Approx 0.55 sec after ejection, drogue gun fires, 22 in. dia then 5 ft dia drogues deploy to
  stabilise and slow seat
Above 5000 m (16000 ft)
  - barostat prevents operation of time-release mechanism
Below 5000 m (16000 ft), low speed
After delay of 2 secs to give time for speed to decrease, the barostatic time-release unit operates to -
  - release parachute harness from seat locks
  - release scissor shackle to release drogues and commence parachute deployment
Main parachute deploys, aircrew separates from seat after being held momentarily by
  sticker straps. Action of sticker straps ensures divergence of aircrew and seat
Operation of auxiliary parachute pulls parachute hard shell clear of area
Normal parachute descent
Manual lowering of personal survival pack
Manual initiation of liferaft inflation (when carried)
Manual separation system available if necessary. Operation of manual separation handle
  releases parachute harness, negative-g strap, PEC and leg restraint cords. Parachute
  withdrawal ine is severed, freeing parachute from seat. Aircrew can then use rip cord to
  operate parachute

Variants

Country
Aircraft
Seat Designation
 
 
 
CANADA
F-18
SJU9A(Rear/Solo)
ECAUDOR
JAGUAR
EB9
FRANCE
Nord 500
FRN9
GERMANY
Dornier DO31
GD9
GERMANY
VAK 191
GV9
INDIA
JAGUAR
IN9B MkIII
INDIA
JAGUAR
IN9B
NIGERIA
JAGUAR
NGB9
OMAN
JAGUAR
OB9
U.K
JAGUAR
9B
U.K
HARRIER
9A
U.K
JAGUAR
9B
U.K
JAGUAR
9B Mk3
U.K
Harrier
9D1
U.K
HARRIER
9D2
U.K
JAGUAR
EB9
U.K
HARRIER
9D

 

Mk. 9
  9B MK3 Jaguar