 |
|||
|
|
|||
| ||||||||||
|
| MIL-D-23222A (AS)
REFERENCES. - Any reference to "NAVAIR" herein
6.4.2
shall mean the "Naval Air System Command". Any
reference to "NAVPRO" herein shall mean the "Navy Plant Representative
Office".
DEFINITIONS. - The following terms and symbols are
6.4.3
defined for use or reference herein.
6.4.3.1
WEIGHTS
BASIC DESIGN GROSS WEIGHT. - The basic design gross
6.4.3.1.1
weight shall be that weight specified in the detail
specification for the flight or landing as the specific test under
consideration may require.
MAXIMUM DESIGN GROSS WEIGHT. - The maximum design
6.4.3.1.2
gross weight shall be that" weight specified in the
detail specification for flight or landing as the specific test under
consideration may require.
SPEEDS. - Speeds shall be in knots based upon the
6.4.3.2
international nautical mile.
6.4.3.2.1
EQUIVALENT AIRSPEED (EAS).- The true airspeed multi-
plied by the square root of the density ratio at
the altitude concerned.
DIVE. - The term "dive" in a broad sense refers to
6.4.3.3
a flight executed for the purpose of demonstrating
strength and rigidity.
6.4.3.4
EXTERNAL STORES. - The term "external stores" means
any item, except streamed tow targets, mounted ex-
ternally on and releasable from the helicopter during flight.
6.4.3.5
Limit. - The term Whit" used in such phrases as
"limit load factor", "limit side load factor", and
"limit dive speed" refers to the design limit specified in applicable
design specifications.
6.4.3.6
MAXIMUM SAFE. - The expression "maximum safe load
(or speed)" means the maximum load factor (or speed)
at the specified speed (or load factor) which can be obtained without
exceeding the specified limit strength or limits for satisfactory
stability and control.
117
|
|
Privacy Statement - Press Release - Copyright Information. - Contact Us |
Click
here for thousands of PDF manuals