 |
|||
|
|
|||
| ||||||||||
|
|  MIL-S-18471G(AS)
APPENDIX
30.5 Ejection test reports. For each DT-IA (see 4.3.c and 4.3.d),
DT-IB and DT-IIB ejection test, the final report required by 4.7.3.3.3
shall include the standard escape trajectory plot for the test see figure
10), the updated composite standard escape trajectory plots for each test
series, parachute damage charts (see figures 11 and 12) for all recovery,
stabilization or other system parachutes, dummy damage charts (see figures
13 and 14), and equipment damage charts (see figures 15 and 16). The standard
escape trajectory plot (see figure 10) shall note all major events including,
but not limited to, the following as applicable:
a. Escape system initiation.
b. Aircraft canopy first motion or aircraft canopy severance.
c. Ejection seat first motion.
d. Catapult ignition.
e. Aircraft canopy clear of escape path.
f. Rocket ignition.
g. Catapult separation.
h. Start of each stabilizer/deceleration action.
i. Rocket burnout.
j. Completion of each stabilizer/decelerator action.
k. Aircrewmember-ejection seat separation.
l. Recovery subsystem initiations.
Recovery subsystem parachute container opening.
n. Recovery subsystem parachute canopy full line stretch.
o. Recovery subsystem parachute canopy first full open.
p. Achievement of steady state descent, as defined in 3.2.2.6.1.e.
Ejection test reports shall be prepared in the format described in figure 17.
88
|
|
Privacy Statement - Press Release - Copyright Information. - Contact Us |
Click
here for thousands of PDF manuals