Table 1: Effective areas and transmission factors of the SPI gamma-ray camera for the observation conditions of the flare obtained by MGGPOD simulations with a detailed model of SPI and the spacecraft.
$E_{\gamma}$ (keV) origin eff. area (cm2) transmission (%)
1369 24Mg $^{\star}_{1369}$ 3.6 2.8
1634 20Ne $^{\star}_{1634}$ 4.6 4.0
1779 28Si $^{\star}_{1779}$ 5.0 4.5
2223 1H(n,$\gamma$)2H 5.4 5.7
4438 12C $^{\star}_{4439}$ 5.2 8.7
6129 16O $^{\star}_{6130}$ 4.1 9.3
6916 16O $^{\star}_{6917}$ 3.6 9.4
7115 16O $^{\star}_{7117}$ 3.6 9.4


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