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Table 2

Shape of three possible bow shocks (from fitting Eq. (22) of Ostriker et al. 2001).

Knot ID υs (km s−1) Cs (Ions−1) β θ (º) Rj (au) α (º)
A1 150 8 4.1 141.15 1237 4
B2 150 8 4.1 −30.4 469 5.5
C1 150 8 4.1 −49.25 349 2

Notes. Column 2: assumed bow-shock speed; Col. 3: assumed sound speed; Col. 4: assumed β; Col. 5: jet axis position angle; Col. 6: inner jet radius; Col. 7; angle to the driving source subtended by Rj.

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