 |
|||
|
Page Title:
Table IV. Mission Conditions Envelope |
|
||
| ||||||||||
|
|  MIL-N-81604C(AS)
Para 3.4.1.1 (cont)
d.
INS (Inertial)
e.
MAG SLV (Magnetic Slaved)
f.
FREE (Platform Free)
g.
EM MAG (Emergency Magnetic)
The equipment shall be capable of operating in any mode without
*
restriction as to having first been in any other particular mode,
except that the equipment must be switched to OFF prior to enter-
ing NORM or INS from the MAG SLV, FREE, or EM MAG modes. It
shall be possible to switch modes, including the BIT mode, with-
out damaging the equipment. There shall be detents which require
the CIU mode switch to be pulled out when switching from OFF to
BIT, from NORM to OFF, and from INS to MAG SLV.
TABLE IV.
MISSION CONDITIONS ENVELOPE
Parameter
Range
Latitude Range (degrees)
S90 to N90
Longitude Range (degrees)
W180 to E180
Groundspeed Range (ft/see)
0 to 3000
Aircraft Roll Attitude (degrees)
-180 to +180
Aircraft Pitch Attitude (degrees)
-90 to +90
Aircraft Heading (degrees)
0 to 360
Roll Angular Rate (degrees/see)
0 to
300
*Pitch Angular Rate (degrees/see)
0 to
60
Yaw Angular Rate (degrees/see)
0 to
200
2
Roll Angular Acceleration (degrees/sec )
0 to
1500
2
Pitch Angular Acceleration (degrees/sec )
0 to
200
2
Yaw Angular Acceleration (degrees/sec )
0 to
200
2
Linear Acceleration Range (ft/sec )
0 to
307.2
Mission Duration (hours)
0 to
6.0
*Within 15 of the zenith and nadir, the maximum pitch
angular rate shall be 35 per second.
20
|
|
Privacy Statement - Press Release - Copyright Information. - Contact Us |
Click
here for thousands of PDF manuals