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Aldrin classic Earth-Mars cycler (inbound / down-escalator, 1 synodic)

aldrin-classic-em-k1-inbound · source: literature · validation: V0

Signature

Bodies
M-E
Sequence (canonical)
M-E
Sense
inbound
Period
2.135 yr (1 × E-M synodic)
Priority date
1985-10-28

V∞ at encounters

M (#1)
9.70 km/s
Due to symmetric geometry, the inbound V_inf matches the outbound V_inf. Value from Russell 2004 Table 3.4 for the Aldrin.
E (#2)
6.50 km/s
Symmetric with outbound.

Orbit elements (heliocentric)

Semi-major axis a
1.600 AU
Eccentricity e
0.393
Perihelion
0.970 AU
Aphelion
2.230 AU
Inclination
0.00°

Orbital elements are identical to the outbound escalator (Rogers et al. 2012 Table 1).

Legs

Primary citation

Aldrin, B. (1985). Cyclic Trajectory Concepts. SAIC presentation to the Interplanetary Rapid Transit Study Meeting, JPL.

Notes

The "inbound" / "down escalator" branch. Time-mirror image of `aldrin-classic-em-k1-outbound`. While M7 novelty matching will likely collapse this under the same primary identity as the outbound, it is given a dedicated seed so the search algorithm validates both directional geometries explicitly.

Source quotes (per-field provenance)

Every numerical value in this entry traces to a verbatim or paraphrased quote from a cited source.

a_au
Rogers et al. 2012, Table 1: 'Aldrin Cycler ... Semi-Major Axis, AU: 1.60'.
e
Rogers et al. 2012, Table 1: 'Aldrin Cycler ... Eccentricity: 0.393'.
perihelion_au
Rogers et al. 2012, Table 1: 'Aldrin Cycler ... Perihelion Radius, AU: 0.97'.
aphelion_au
Rogers et al. 2012, Table 1: 'Aldrin Cycler ... Aphelion Radius, AU: 2.23'.
vinf_kms_at_encounters[0].vinf_kms
Russell 2004 dissertation §3.8: 'Due to symmetry, the energy properties for inbound and outbound cyclers are identical.'
vinf_kms_at_encounters[1].vinf_kms
Russell 2004 dissertation §3.8 (same as above).
legs[0].tof_days
Wikipedia / McConaghy 2002: symmetric 146-day fast transit.
period.years
Earth-Mars synodic 2.135 yr — spec.md §9.