IEEE Aerospace and Electronic Systems Magazine - July 2020 - 13

Davarian et al.

Figure 2.
Uplink data rate as a function of range.

A NOTE ON KA-BAND LINK PERFORMANCE

EMERGENCY MODE

In the above section, spacecraft-to-Earth Ka-band link
performance was evaluated at a low elevation angle of 20
that exaggerates atmospheric-related losses (X-band is
less susceptible to losses resulting from propagation
through the atmosphere than Ka-band). This assumption
coupled with other presumed losses, such as circuit,
antenna pointing, etc., may present a conservative picture
of Ka-band performance for mission planners who need to
decide between Ka- or X-band for their mission. Empirical
data based on the long-term observations of deep space
Ka-band links of Cassini and Kepler missions were analyzed to provide a performance estimate for mission planners and designers [1]. The resulting model not only
accounts for weather, it also includes other link losses that
are difficult to identify. Therefore, at the onset of mission
planning, it may be beneficial to apply the model provided
in [1] to evaluate the utility of Ka-band for the mission
of interest.

Emergency mode communications uses the X-band to avoid
weather-related losses, and assumes a low-gain antenna
onboard the spacecraft to prevent the need for accurate
pointing while in emergency. In this study, it is assumed that
the emergency mode rate is 10 b/s. Figure 3 shows the downlink margin in emergency mode as a function of range;
assumptions for the link are shown in Table 7. Similar to the
previous two figures, a number of targets have been shown

Table 6.

Assumptions for Figure 2
Spacecraft

CubeSat

MicroSat

Receive antenna gain

28.5 dBi

38.5

Noise figure

3 dB

3 dB

Elevation

20

20

DSN antenna

34 m

34 m

Weather

90%

90%

Command mod
index

1.5 rad

1.5 rad

Command data rate

Variable

Variable

Frequency

7150 MHz

7150 MHz

Modulation

BPSK

BPSK

Coding

Uncoded

Uncoded

Ground

UPLINK (EARTH TO SPACECRAFT)
Because the DSN antennas are very powerful transmitters,
the uplink scenario for SmallSats is more promising than
the downlink. Figure 2 illustrates uplink data rate values
of CubeSats and MicroSats as a function of distance;
assumptions for the link are shown in Table 6. It is
assumed that the uplink uses X-band to avoid weatherrelated losses associated with Ka-band. Color codes correspond to the same targets, as shown in Figure 1. SmallSats
can meet the requirement of 1 kb/s uplink data rate even
at Jovian distances. Therefore, the takeaway from this
chart is that SmallSats are not uplink limited.
JULY 2020

Link

IEEE A&E SYSTEMS MAGAZINE

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IEEE Aerospace and Electronic Systems Magazine - July 2020

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