Central Optic Tech

MS-30

Issuing time:2025-01-16 14:52

Parameter：

Weight：30 kg

Payload：20 kg

Life time：5 years

Pointing Accuracy：0.05°

Satellite Orbit：LowEarth Orbit

Standardized low-cost platform, rapiddevelopment and delivery

Modular design, flexible configuration tomeet customized needs

Three-axis stability control

Orbital maintenance System

Low power consumption on-orbit standbyfunction

Suitable for many types of loads

Suitable for medium-resolution remotesensing of the earth

Suitable for low earth orbit constellations

Suitable for communication, navigation andtechnical experiments, etc.

Attitude Accuracy	0.001°
Pointing Accuracy	0.05°
Attitude Stability	0.01°/s
Maximum Angle Velocity	3°/s
Side Swing Range	±35°
Long Run Mode	Sun cruise, three-axis stability of the earth, low-power consumption magnetron to the sun
Work Mode	Ground gazing, ground sweep, space target gazing, Space Pointing

Detailed Configuration：

Star Tracker	Quantity	3
	Accuracy	5”
	Dynamic Range	2 °/s
	Update Rate	10 Hz
Sun Sensor	Quantity	2
	Accuracy	0.1°
	Update Rate	5 Hz
	Field of View	88°×100°
Gyroscope	Equipment	MEMS-A	MEMS-B
	Bias Stability	0.1°/h	0.5°/h
	Angle Random Walk	0.05°/√h	0.025°/√h
	Update Rate	20 Hz	20 Hz
Magnetometer	Quantity	2
	Measuring Range	±1 Gauss
	Magnetic Field Identification	0.2 mGauss
	Update Rate	10 Hz
Reaction Wheel	Quantity	4+3(Standby)
	Angular Momentum	300 mNms
	Speed Control Accuracy	±1 rpm
	Rated Speed	6000 rpm
	Force Momentum	10 mNm
Magnetic Torquer	Quantity	3
	Magnetic Moment	5 Am2
	Residual Magnetic Moment	<3%
	Linearity	<5%
GNSS	Positioning Accuracy	10 m
	Speed Measurement Accuracy	0.1 m/s
	Time Scale Precision	100 ns
Propulsion	Impulse	800 Ns
	Thrust	10 mN
	Propellant	Liquid Ammonia

ADD：1921-1922, 2#Building, 26# Chengtong Street, Shijingshan District, Beijing 100043 P.R.China.

Postal Code：100043

Tel：+010-53679777

E-mail：info@centraloptictech.com