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Table 1

Parameters used in the EDCM for the CI mission target.

Symbol Unit Parameter Value/range/function Step size
Nucleus parameters

rh au Heliocentric distance 1 n/a
RN km Nucleus radius 2, 5 n/a
ρN kg m−3 Bulk density of the nucleus 317, 508 n/a
Tn K Nucleus surface temperature at the sub-solar point 317 n/a
q(φ) Gas emission distribution (~cosk(φ)) k = 1, 2, 3 n/a
s−1 Global gas production rate for an equivalent sphere with 1.3 × 1027−4.9 × 1028 Uniformly sampled
Relative night side activity 0.01, 0.05, 0.1 n/a

Dust particle parameters

a m Radius 10−6–10−1 Half decade
ϱd(a) kg m−3 Bulk density 300–1000 100
qrad(a) Radiation pressure efficiency 0.2–2 ~0.1
qsca(a) Scattering efficiency Silicates & Organics(*) n/a
ϕ(α) Phase function Silicates & Organics(*) n/a

Dust coma parameters

Afρ cm Brightness 2800–28 000 2000
β Differential power law exponent of the dust size 3.2–4.4 0.2
distribution; n ~ aβ
χ(*) Dust-to-gas mass production rate ratio <10 n/a

S/C trajectory parameters

rCA km Cometocentric distance of spacecraft at closest aThe closest approach (CA) distance, the trajectory angle in the meridional plane, αT, and the trajectory angle in the equatorial plane, βT. pproach (CA) 1000, 500, 200 for S/C A,B1, B2
αT deg Trajectory angle in the meridional plane 0 n/a
βT deg Trajectory angle in the equatorial plane 0 n/a

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