TM 9-1550-416-14&P
Table 1-1. Equipment Description and Data
Data
Item
PERFORMANCE
Maximum 46 MPH at sea level with zero wind.
Speed
Minimum 29 MPH at sea level with zero wind.
Minimum of 10 minutes at maximum speed.
Endurance
Three kilometers maximum
Range
Operational Altitudes
Sea level to maximum of 10,000 feet above sea level.
Roll rate at full throttle is minimum of 180 degrees per
Maneuverability
second from level of flight at all operational altitudes.
Pitch rate at full throttle is minimum of 60 degrees per
second from level flight at all operational altitudes.
Launch Method
Hand launch in winds up to 25 knots.
Under the conditions of unimproved grassy and/or sandy
Survivability
areas normally found at training and firing ranges, the
airborne system is recoverable with a minimum of struc-
tural damage.
Excluding hits to the engine, fuel, tank, electronics and
control mechanisms, the airborne system can survive a
small arms hit up to 20 millimeters in size with minimal
operational degradation.
ANCILLARY DEVICES
The airborne system is capable of accommodating a 5 pound,
80-cubic-inch (typical 2.0 inches by 4.0 inches by 10
inches long) payload of uniform density. The payload will
not degrade performance characteristics and is carried
internally in a payload compartment, or externally. The
airborne system will permit a radar signature sufficient
for VULCAN ROR (9145 to 9185 MHz) to engage and lock
at 500 meters.
F-16
Mig-27
PHYSICAL DIMENSIONS
44.0 inches
68.0 inches
Wingspan
Aerial Target
62.0 inches
72.0 inches
Length
6 pounds 3 ounces
7 pounds 0 ounces
Weight
without fuel
without fuel
7.75 inches
Width
3.125 inches
Depth
9.25 inches
Height
5 pounds 10 ounces
Weight
Collapsed: 8.5 inches
Length
Fully extended: 101 inches
51.0 inches
Receiver Antenna
Length
Support Equipment- GSE
Width
22.25 inches
Field Box
7.25 inches
Depth
11.5 inches
Height
Approximately 25 pounds with start-
Weight
er and battery installed
1-3
