Research Article

AOCS Requirements and Practical Limitations for High-Speed Communications on Small Satellites

Table 22

Link budget for satellite with an orbit height between 400 km and 900 km.

Parameter
10°15°10°15°

Comm. systemData rate (Gbps)1.501.501.501.50
Wavelength (nm)1550155015501550
Modulation formatIntensity modulation and direct detection
Bit error rate1.0E − 061.0E − 061.0E − 061.0E − 06

TXOutput power (dBW)0.000.000.000.00
TX loss (dB)1.491.491.491.49
TX divergence FWHM (mrad)0.0410.0410.0410.041
TX aperture diameter (cm)4.004.004.004.00
TX telescope gain Gt (dB)98.1898.1898.1898.18
(dB)3.013.013.013.01

ChannelLink distance (km)1439117525882224
(dB)261.34259.58266.44265.12
(dB)3.502.503.502.50
(dB)4.003.004.003.00

RXAperture diameter (cm)60.0060.0060.0060.00
RX-telescope gain (dB)121.42121.42121.42121.42
(dB)1.001.001.001.00
Optical RX losses (dB)6.026.026.026.02
RX-power after losses (dBW)−60.76−57.00−65.86−62.54

Sensitivity (dBW)−67.00−67.00−67.00−67.00
Margin with sensitivity (dB)6.2410.001.144.46