SPACE ANTENNAS / COTS
SPACE ANTENNAS / COTS
CSA-S-006-RH
CSA-S-006-RH
S-Band RHCP Isoflux Antenna
S-Band RHCP Isoflux Antenna
CSA-S-006-RH is a COTS S-band isoflux antenna covering 2000 to 2300 MHz, shaping its pattern to concentrate gain at low elevation angles where slant range is longest and link margin is tightest. Peak gain is 0 to 1.7 dBic at 20 to 30 degrees elevation with a 190 to 210 degree half-power beamwidth on the receive band. Developed for lunar missions, RHCP, 20 W handling with 10 dB multipaction margin, TRL 8 at 170 g.
CSA-S-006-RH is a COTS S-band isoflux antenna covering 2000 to 2300 MHz, shaping its pattern to concentrate gain at low elevation angles where slant range is longest and link margin is tightest. Peak gain is 0 to 1.7 dBic at 20 to 30 degrees elevation with a 190 to 210 degree half-power beamwidth on the receive band. Developed for lunar missions, RHCP, 20 W handling with 10 dB multipaction margin, TRL 8 at 170 g.

PRODUCT OVERVIEW
An isoflux pattern compensates for the fact that a ground terminal at the edge of the visible disc is significantly further away than one at nadir, flattening received flux across the pass rather than peaking it at boresight. Wide bandwidth allows simultaneous transmit and receive through a single port, eliminating a second antenna and its cabling. Axial ratio runs 1.3 to 3.3 dB across 2000 to 2120 MHz and 1 to 2.5 dB across 2200 to 2300 MHz, with VSWR at 2:1 through an SMA female interface. The envelope is 97 x 97 x 89 mm (3.8 x 3.8 x 3.5 in) at 170 g. The antenna is built to withstand the harsh conditions of the lunar environment over long mission durations, addressing corona, multipaction and MMOD. Qualification is to NASA GEVS (GSFC-STD-7000) with random vibration to 14.1 GRMS overall across a -70 to +100 °C operating and storage range. ATH-S-004-RH is the matching test hat, shaped around the isoflux geometry to give a repeatable coupling factor during integration.
An isoflux pattern compensates for the fact that a ground terminal at the edge of the visible disc is significantly further away than one at nadir, flattening received flux across the pass rather than peaking it at boresight. Wide bandwidth allows simultaneous transmit and receive through a single port, eliminating a second antenna and its cabling. Axial ratio runs 1.3 to 3.3 dB across 2000 to 2120 MHz and 1 to 2.5 dB across 2200 to 2300 MHz, with VSWR at 2:1 through an SMA female interface. The envelope is 97 x 97 x 89 mm (3.8 x 3.8 x 3.5 in) at 170 g. The antenna is built to withstand the harsh conditions of the lunar environment over long mission durations, addressing corona, multipaction and MMOD. Qualification is to NASA GEVS (GSFC-STD-7000) with random vibration to 14.1 GRMS overall across a -70 to +100 °C operating and storage range. ATH-S-004-RH is the matching test hat, shaped around the isoflux geometry to give a repeatable coupling factor during integration.
TECHNICAL SPECIFICATIONS
RF PERFORMANCE
FREQUENCY RANGE
2025-2300 MHz
PATTERN
Isoflux
POLARIZATION
RHCP
GAIN
1 dB
RF POWER HANDLING
43 dBm
INTEGRATION & QUALIFICATION
APPLICATION
TT&C
TRL
TRL 8
OPERATING TEMPERATURE
-70 to +100 °C
HUMIDITY
VIBRATION
14.1 GRMS random (GSFC-STD-7000)
SHOCK
MASS
170 g
COMPATIBLE COTS TEST HAT
ATH-S-004-RH