PA-RR-206

Pegasus
Actuators GmbH
WHERE PRECISION &
RELIABILITY SOAR
From single
components to
entire propulsion
systems
and innovative
defense networks –
our main focus
is in engines,
components and
support solutions
for any UAV or
unmanned system.
SERVO
ACTUATORS
Redundant PA-RR-260-8
Pegasus
REDUNDANT
PA-RR-260-8
UAV Servo
Actuator
“tough tech for tough environments“
UAV SERVO ACTUATOR
Actuators GmbH
We have done
the research.
We have done
the testing.
We will build it,
test it and
deliver it to you,
ready to fly.
w w w. p e g a s u s - a c t u a t o r s . c o m
“Tough tech for tough environments”
AGENC
Y

AS9100
ACT A
U
ENSE
C
EF
D
TR
N
O

TM
IT
D
BSI
WEST COAST DISTRIBUTOR
PEGASUS Servo Actuators are electromechanical drive units of extraordinary
power density, precision and reliability, they are installed in industrial and remotely
controlled employments where exceptional precision and reliability are imperative.
NWUAV is the distributor West of the Mississippi for the Pegasus UAV Servo
Actuator product-line. Pegasus offers a wide range of affordable Servo
Pegasus
“tough tech for tough environments“
Actuators for multiple rotary and fixed wing UAV applications from 30 lbs
Pegasus
REDUNDANT PA-RR-260-8
A c tUAV
u aSERVO
t o r ACTUATOR
s G m b H Aup
c t u a to
t o r s 1000
G m b H lbs maximum takeoff weight (MTOW).
SUPPLY DATA
Operating Voltage
18V - 32V
Operating Voltage Typical24V
Standby Current250mA
Input Signal
Redundant RS485 data protocol
POSITION FEEDBACK SELECTION
Analog 0-5V or 0-10V differential
PWM 0-5V differential
RS485 0-5V differential
PERFORMANCE DATA
Stall Torque
> 500 Ncm / > 710 oz-in.
Rated Torque**
300 Ncm / 425 oz-in.
Speed at Rated Torque135°/sec.
Redundant PA-RR-260-8
UAV Servo Actuator
w w w. p e g a s u s - a c t u a t o r s . c o m
No Load Speed190°/sec.
PRODUCT FEATURES
• Redundant PA-ME³ magnetic deflection
angle sensor
• Dual brushless motors
• Dual servo controller PCB
• Dual Glenair Mighty Mouse Series 801,
7-pin connector
• Single Point Failure redundancy architecture
• Oil lubricated gear-box
• Unparalleled anti flutter circuit
• Enhanced positioning resolution
• Inbuilt (switchable) termination resistor
• Inbuilt safeguarding fuses
• Inbuilt power supply filter
• Enhanced feedback signal resolution
Gear Train Backlash
< 0,5°
Travel Angle standard ± 90°
Max. Travel Angle (optional)
± 170°
Pa-Sc Release Point
500Ncm / 710 oz-in.
Peak Current - Short Time1950mA
Stall Current - Continuous
1150mA (limited)
Weight
430g /15 oz
ENVIRONMENTAL DATA
Axial Load On Output Shaft
< 100N
Lateral Load On Output Shaft < 300N
Operating Temperature
-40°C - +70°C
Storage Temperature
-40°C - +85°C
ENVIRONMENTAL SPECIFICATIONS
DO-160 F (RCTA)
MIL-STD-810G
**according Pegasus Actuators GmbH specs.(please inquire the test-specifications)
WEST COAST DISTRIBUTOR
TM
www.nwuav.com
11160 SW Durham Lane, Suite 1 | McMinnville, OR 97128 | Office: 503.434.6845 | Fax: 503.217.6080
The materials contained in this brochure are provided for information only, “as is” without any warranties, express or implied, including warranties of merchantability, fitness of purpose and non-infringement of third-party intellectual property. While every effort is
made to ensure that the information and specifications are accurate, the scope of information is limited by nature. NWUAV Propulsion Systems reserves the right to make changes to the Products described in the Product Brochure at any time, without notice. The
application of our products is dependent upon the operating mission, environmental conditions, loads and other factors; none of which can be ascertained by this brochure. Any technical advice or information gleaned from this Product Brochure is given in good
faith and without charge, and said advice and information is provided by NWUAV Propulsion Systems without assumption of liability or obligation. This brochure and the information it contains is the work product of NWUAV Propulsion Systems (“NWUAV”). All
title, ownership rights and intellectual property rights in and relating to this brochure is owned by NWUAV or used by NWUAV through pre-authorization by third parties and cannot be used without its express prior written permission.

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