APEX Antenna Efficiencies

2017	2018	2019	2020	2021	2022	2023

Mars	Jupiter	Uranus	All

Instrument	Year-Month	Planet	θS ('')1	Frequency (GHz)	θmb ('')	ηa2,4	ηmb3,4	Jy/K5	# Scans
LASMA345	2024-11	MARS	10.2 ± 0.00	332.70	18.2	0.63 ± 0.05	0.77 ± 0.06	39 ± 3	8
LASMA345	2024-11	MARS	10.2 ± 0.00	344.70	17.6	0.61 ± 0.05	0.74 ± 0.06	40 ± 3	8
LASMA345	2024-11	MARS	9.9 ± 0.23	333.80	18.1	0.64 ± 0.05	0.79 ± 0.06	37 ± 3	28
LASMA345	2024-11	MARS	9.9 ± 0.23	345.80	17.5	0.62 ± 0.05	0.77 ± 0.06	39 ± 3	28
NFLASH230	2024-10	URANUS	3.7 ± 0.01	218.37	27.7	0.65 ± 0.05	0.80 ± 0.07	37 ± 3	8
NFLASH230	2024-10	JUPITER	43.4 ± 0.18	210.63	28.7	0.69 ± 0.06	0.85 ± 0.07	35 ± 3	8
NFLASH230	2024-10	JUPITER	43.3 ± 0.72	218.37	27.7	0.67 ± 0.06	0.83 ± 0.07	36 ± 3	8
NFLASH230	2024-10	URANUS	3.7 ± 0.01	230.71	26.2	0.66 ± 0.05	0.81 ± 0.07	36 ± 3	8
NFLASH230	2024-10	JUPITER	43.4 ± 0.18	222.97	27.1	0.72 ± 0.06	0.88 ± 0.07	33 ± 3	8
NFLASH230	2024-10	JUPITER	43.3 ± 0.72	230.71	26.2	0.69 ± 0.06	0.85 ± 0.07	35 ± 3	8
NFLASH230	2024-10	MARS	8.0 ± 0.39	218.37	27.7	0.63 ± 0.05	0.77 ± 0.06	38 ± 3	22
NFLASH230	2024-10	MARS	8.0 ± 0.39	230.71	26.2	0.64 ± 0.05	0.79 ± 0.06	38 ± 3	22
SEPIA660	2024-09	MARS	7.1 ± 0.20	685.17	8.6	0.39 ± 0.03	0.46 ± 0.03	62 ± 4	14
NFLASH230	2024-09	MARS	7.1 ± 0.22	218.37	27.7	0.62 ± 0.05	0.76 ± 0.06	39 ± 3	78
NFLASH230	2024-09	JUPITER	39.4 ± 0.61	218.37	27.7	0.67 ± 0.05	0.82 ± 0.07	36 ± 3	20
NFLASH230	2024-09	MARS	7.1 ± 0.22	230.71	26.2	0.63 ± 0.05	0.78 ± 0.06	38 ± 3	78
SEPIA345	2024-09	MARS	6.6 ± 0.06	278.83	21.7	0.65 ± 0.05	0.80 ± 0.07	37 ± 3	6
NFLASH230	2024-09	JUPITER	39.4 ± 0.61	230.71	26.2	0.69 ± 0.06	0.85 ± 0.07	35 ± 3	20
SEPIA660	2024-09	MARS	7.1 ± 0.20	672.83	8.8	0.39 ± 0.03	0.46 ± 0.03	62 ± 4	14
SEPIA345	2024-09	MARS	6.6 ± 0.06	291.17	20.8	0.67 ± 0.06	0.82 ± 0.07	36 ± 3	6
LASMA345	2024-08	MARS	6.1 ± 0.13	271.35	22.3	0.67 ± 0.05	0.82 ± 0.07	36 ± 3	12
NFLASH230	2024-08	MARS	5.9 ± 0.00	237.83	25.4	0.58 ± 0.05	0.71 ± 0.06	42 ± 3	6
NFLASH460	2024-08	MARS	6.0 ± 0.00	473.21	12.8	0.47 ± 0.04	0.58 ± 0.05	51 ± 4	8
NFLASH230	2024-08	URANUS	3.6 ± 0.01	230.71	26.2	0.65 ± 0.06	0.80 ± 0.07	37 ± 3	12
SEPIA345	2024-08	MARS	6.3 ± 0.01	278.83	21.7	0.69 ± 0.06	0.84 ± 0.07	35 ± 3	8
LASMA345	2024-08	MARS	6.1 ± 0.13	283.35	21.4	0.67 ± 0.06	0.82 ± 0.07	36 ± 3	12
LASMA345	2024-08	MARS	6.1 ± 0.14	333.80	18.1	0.64 ± 0.05	0.78 ± 0.07	38 ± 3	20
NFLASH230	2024-08	MARS	6.0 ± 0.00	250.37	24.2	0.57 ± 0.05	0.70 ± 0.06	42 ± 3	8
NFLASH230	2024-08	MARS	5.9 ± 0.00	250.17	24.2	0.59 ± 0.05	0.73 ± 0.06	41 ± 3	6
NFLASH460	2024-08	MARS	6.0 ± 0.00	460.87	13.1	0.50 ± 0.04	0.61 ± 0.05	49 ± 4	8
NFLASH230	2024-08	MARS	6.2 ± 0.19	218.37	27.7	0.62 ± 0.05	0.76 ± 0.06	39 ± 3	40
SEPIA345	2024-08	MARS	6.3 ± 0.01	291.17	20.8	0.71 ± 0.06	0.87 ± 0.07	34 ± 3	8
LASMA345	2024-08	MARS	6.1 ± 0.14	345.80	17.5	0.62 ± 0.05	0.76 ± 0.06	39 ± 3	20
NFLASH230	2024-08	MARS	6.0 ± 0.00	262.71	23.0	0.56 ± 0.05	0.69 ± 0.06	43 ± 4	8
NFLASH230	2024-08	MARS	6.2 ± 0.19	230.71	26.2	0.63 ± 0.05	0.78 ± 0.06	38 ± 3	40
NFLASH230	2024-08	URANUS	3.6 ± 0.01	218.37	27.7	0.65 ± 0.05	0.80 ± 0.07	37 ± 3	12
LASMA345	2024-07	MARS	5.6 ± 0.13	333.80	18.1	0.64 ± 0.05	0.78 ± 0.06	38 ± 3	44
LASMA345	2024-07	MARS	5.6 ± 0.13	345.80	17.5	0.62 ± 0.05	0.76 ± 0.06	39 ± 3	44
NFLASH230	2024-06	MARS	5.2 ± 0.08	218.37	27.7	0.63 ± 0.05	0.78 ± 0.06	38 ± 3	22
LASMA345	2024-06	MARS	5.2 ± 0.17	333.80	18.1	0.64 ± 0.05	0.79 ± 0.06	37 ± 3	20
NFLASH230	2024-06	MARS	5.1 ± 0.01	267.17	22.7	0.54 ± 0.04	0.67 ± 0.05	44 ± 4	10
SEPIA345	2024-06	MARS	5.1 ± 0.02	350.46	17.3	0.59 ± 0.05	0.73 ± 0.06	41 ± 3	12
NFLASH230	2024-06	MARS	5.2 ± 0.08	230.71	26.2	0.65 ± 0.05	0.79 ± 0.06	37 ± 3	22
SEPIA345	2024-06	MARS	5.1 ± 0.06	278.83	21.7	0.67 ± 0.05	0.82 ± 0.07	36 ± 3	30
LASMA345	2024-06	MARS	5.2 ± 0.17	345.80	17.5	0.63 ± 0.05	0.77 ± 0.06	39 ± 3	20
SEPIA345	2024-06	MARS	5.1 ± 0.02	362.80	16.7	0.56 ± 0.05	0.69 ± 0.06	43 ± 4	12
SEPIA345	2024-06	MARS	5.1 ± 0.06	291.17	20.8	0.69 ± 0.06	0.85 ± 0.07	35 ± 3	30
NFLASH230	2024-06	MARS	5.1 ± 0.01	254.83	23.8	0.55 ± 0.04	0.67 ± 0.06	44 ± 4	10
NFLASH230	2024-05	MARS	4.8 ± 0.09	218.37	27.7	0.64 ± 0.05	0.79 ± 0.06	38 ± 3	24
NFLASH230	2024-05	MARS	4.8 ± 0.09	230.71	26.2	0.66 ± 0.05	0.80 ± 0.07	37 ± 3	24
NFLASH460	2024-04	MARS	4.6 ± 0.01	473.21	12.8	0.50 ± 0.04	0.61 ± 0.05	49 ± 4	8
NFLASH460	2024-04	MARS	4.6 ± 0.01	460.87	13.1	0.49 ± 0.04	0.60 ± 0.05	49 ± 4	8
NFLASH230	2024-04	MARS	4.6 ± 0.06	218.37	27.7	0.64 ± 0.05	0.78 ± 0.06	38 ± 3	38
NFLASH230	2024-04	MARS	4.6 ± 0.06	230.71	26.2	0.65 ± 0.05	0.80 ± 0.07	37 ± 3	38

Note 1: The planet sizes (θ_S) and fluxes from the planet models usually have < 5% uncertanties. The values given in the table above are the average planet size from selected scans (at least 5 scans at a given frequency; for data older than 2018, a minimum of 3 scans is used instead since there was no systematic observations of antenna efficiencies back then). If the planet size is smaller than 0.4 x HPBW (θ_mb) then θ_S, aperture efficiency (η_a) and the point source sensitivity (Jy/K) will be highlighted since the correction [1-exp(-Q)]/Q (with Q=ln(2)(θ_S/θ_mb)²) for non-pointlike source is < 5%.

Note 2: The aperture efficiency (η_a) intrinsicly includes the effects due to error beams, blockage, spillover, etc., because it is measured on sky toward a planet. Thus, it is lower than the expected aperture efficiency due exclusively to the surface accuracy as described by the original Ruze equation.

Note 3: Although the correction for the influence of the source size mentioned in Note 1 is only a first order correction (i.e, it asumes a clean Gaussian beam and does not take into account the effect of the sidelobes nor the error beams), we can consider our estimates a good approximation of the actual main beam efficiency (η_mb).

The spectra delivered by the APEX real-time calibration software (Muders et al. 2006, A&A, 454, L25) is in GILDAS/CLASS format (Pety J., 2005, in SF2A-2005, p. 721) in the corrected (for atmospheric attenuation, the forward efficiency and signal band gain) antenna temperature T_A^* scale (Ulich & Haas, 1976, ApJ, Suppl. Ser., Vol. 30, p. 247). The forward efficiency (η_fw) in the header is set to the actual value (<1.0). The beam efficiency (η_mb) is set to 1.0. In order to switch to the T_MB scale, one needs to multiply the data by η_fw/η_mb. Any further modification of η_mb after this switch of scale needs a multiplication by η_{mb_old}/η_{mb_new}. The "MODIFY BEAM_EFF" command in CLASS does the latter, i.e. it will use the existing eta_beam (=BEAM_EFF) as η_{mb_old} and the supplied value as η_{mb_new}. That is why the first step to switch to T_MB needs an initial BEAM_EFF set to FORWARD_EFF. Hence, for conversion of APEX data to main beam brightness temperature T_MB scale, we recommend using this CLASS script, after loading the data and getting a scan in the CLASS environment.

For point-like (relative to the beam size) science targets we recommend to use the η_mb values estimated from observations towards Uranus or Mars (when smaller than 0.4 x HPBW). For semi-extended sources (not point-like but unresolved by the beam) values estimated from Mars (when 0.4 x HPBW < θ_S < HPBW) are better. For extended sources (resolved by the beam) the values estimated from Jupiter or Mars (when larger than the beam) are recommended.

Note 4: Because of the new sub-reflector the forward efficiency (η_f=0.95) for 2018+ have smaller uncertainty of about 5% in contrast to the 10% uncertainty considered for previous years. Other efficiencies (η_a, η_mb and Jy/K) include the uncertainties of: the forward efficiency, the planet model (4%), the beam size (5%) and the uncertainty of the observed peak brightness temperature (usually < 10% for Uranus, and < 5% for Mars and Jupiter).

Note 5: The Jansky to Kelvin conversion factor for the APEX antenna can also be approximated by η_f24.4/η_a (Jy/K). According to the Ruze formula the aperture efficiency (η_a) and, hence, the main beam efficiency (η_mb), will degrade with shorter wavelength, λ, as

η_a (λ) = η_a (∞) exp(-16π²σ²/λ²)

where σ is the antenna surface RMS value (i.e. describing small scale deviations from a perfect surface).

Likewise, according to Downes (1989) the main beam efficiency can be estimated from the aperture efficiency as

η_mb (λ) = 0.8899 [θ_mb/(λ/D)]² η_a

with θ_mb ≈ k λ/D (assuming a Gaussian beam) where k is a factor that depends on the illumination taper and blockage of the aperture (e.g., Christiansen & Högbom 1985; Kraus 1986). For most APEX receivers we found k ≈ 1.17 which correspond to an edge tapering of about 13.9 dB (consistent with the value assumed by Güsten et al. 2006). Thus, the main beam efficiency can be approximated as: η_mb (λ) = 0.8899 (1.17)² η_a.

From the 2018 commissioning we recommend using θ_mb ≈ (9.0 ± 0.1) 658/f_GHz for the full frequency range of SEPIA660.

For the estimates we select only well focused and calibrated pointing scans toward Mars, Jupiter and Uranus (when available; during most of 2017 Mars was in sun avoidance). Pointing scans with offsets smaller than 10% of the beam size are selected for the estimates. Only the cross-scan in Azimuth are used and we discard the scans where the FWHM from the Azimuth and Elevation cross-scans differ by more than 10%. The aparent size and fluxes of the planets for a particular date and frequency are obtained from the corresponding models implemented in CASA ( CASA Guides: Solar System Models; ALMA memo #594). Comparing with other existing models (e.g., in GILDAS/ASTRO and in the work by Lellouch et al., 2006) we found they agree within 15%. Details of the theory and calculations used in our estimates can be found here. For a more elaborated explanation of the formulas we refer to the IRAM 30m internal documents cali_rep.pdf or spatial_response_framework_v1.8.pdf.

Efficiencies for the PI CHAMP+ instrument can be found at the corresponding web page at MPIfR.

The historical table below was adapted from Güsten et al. (2006, A&A 454, L13-L16). Beam sizes (θ_mb) were determined by deconvolving planet scans. The listed efficiencies are forward efficiency (η_f), aperture efficiency (η_a), main beam efficiency (η_mb), and Moon efficiency (η_M). The uncertainties of the listed efficiencies are expected to be 5-10%. For comparison with older values you can still find the former table of antenna efficiencies here.