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Page Title: PARACHUTE DEPLOYMENT ROCKET MOTOR MK 122 MOD 0
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Aviation Structural Mechanic E1&C - How airplanes are built and how to maintain them
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Barostat Assembly

harness straps to retract but prevent them from extending.  When  in  the  normal  unlocked  state, automatic  locks  protect  the  occupant  against  rapid forward  movement  under  high  g-loading. PARACHUTE   DEPLOYMENT   ROCKET MOTOR  MK  122  MOD  0.—   The   parachute deployment  rocket  motor  (PDRM)  (fig.  5-9)  is mounted on the LH main beam of the seat. When initiated by the sequencer, restraint release unit, or  manual  override  (MOR)  system,  the  PDRM extracts  the  personnel  parachute  from  its  stowage by  means  of  a  withdrawal  line  attached  to  the deployment  sleeve. The  PDRM  is  a  sealed  unit.  It  consists  of  a cylindrical   body   that   contains   a   gas-operated secondary cartridge in a breech at the lower end and  a  rocket  with  an  integral  gas-operated  igniter cartridge in a barrel at the upper end. In a parallel connected  chamber  is  an  electrically  initiated primary cartridge. A gas inlet is connected by a gas pipe to the harness release system. Figure 5-9.-Parachute deployment rocket motor (Mk 122 Mod 0). Fitted around the rocket is a sliding stirrup, which is connected to the parachute withdrawal line and is free to slide down the rocket as it leaves the barrel. ELECTRONIC SEQUENCER.— The NACES sequencer assembly (fig. 5-10) is composed of the sequencer, connectors to the interface with pitot static  and  dynamic  pressure  sources,  and  cable loom sleeving. It is mounted across the main beam assembly,  below  the  parachute  assembly.  Upon activation, the sequencer determines the ejection mode  and  controls  the  functions  of  the  drogue release,   parachute   deployment,   and   seat/man separation. BAROSTATIC  RELEASE  UNIT  (BRU).— The barostatic release unit (fig. 5-11) provides a housing  for  the  cartridge  that  provides  the  gas flow  to  initiate  harness  release  and  parachute rocket  deployment.  The  cartridge  is  activated either electrically by the sequencer or by the right- hand start switch (via the delay mechanism). The cartridge   incorporates   an   aneroid   capsule   to prevent   mechanical   initiation   above   a   preset altitude.  The  cartridge  may  also  be  initiated  by operation  of  the  MOR  handle  after  ejection. Figure  5-10.-Electronic  sequencer. 5-10

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