Summary

NewSpace Systems (NSS) offers the NRWA-T2 reaction wheel for small satellite missions. A high performance alternative to a reaction control system, reaction wheels provide spacecraft with control torque by means of momentum exchange between the satellite body and the rotating wheel.

Typically, three to four reaction wheels are needed to provide full three-axis control of a spacecraft and the additional integration of these wheels with external gyroscopes for full three-axis control using inertial rates. With high torque stability, wheel momentum capacity and accuracy speed control; NSS reaction wheels are suitable for small satellite missions requiring accurate pointing.

Key features of NSS reaction wheels include:

  • Wheel torque and momentum capacity suited to client mission requirements
  • Current, speed and torque control
  • Simple digital interface to spacecraft bus
  • Integration with an optional gyroscope for inertial rate control and inertial angle control modes possible
  • Hermetically sealed (not T10)
  • Long demonstrated lifetimes

NSS reaction wheels can be used in a variety of applications, including:

  • High performance three-axis torque and momentum exchange actuators for small satellite missions
  • Momentum bias
  • Inertial rate control for accurate pointing of imagers

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Last updated: 2023-05-12

NRWA-T2 Reaction Wheel

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Specs

mass
2.8 kg
width
150 mm (wheel)
height
150 mm (wheel)
length
70 mm (wheel)
maximum torque
90 mN m
maximum momentum storage
1 N m s (at 1850 rpm and 84 mN m)
1.47 N m s (at 2700 rpm)
rotor moment of inertia
0.0052 kg m^2
speed control accuracy
<1 rpm @ >100 rpm
power consumption
1.7 W (quiescent)
4 W (steady state at 1500 rpm)
4.8 W (steady state at 2600 rpm)
thermal (acceptance)
-10 to 58 C
power supply
28 V unregulated
data interface
RS422
connector type
9-pin D-type Male
mechanical vibration
16.95 gRMS (random)
radiation tolerance
10 krad (component level)

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