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_auRogers et al. 2012, Table 1: 'Aldrin Cycler ... Semi-Major Axis, AU: 1.60'.
eRogers et al. 2012, Table 1: 'Aldrin Cycler ... Eccentricity: 0.393'.
perihelion_auRogers et al. 2012, Table 1: 'Aldrin Cycler ... Perihelion Radius, AU: 0.97'.
aphelion_auRogers et al. 2012, Table 1: 'Aldrin Cycler ... Aphelion Radius, AU: 2.23'.
vinf_kms_at_encounters[0].vinf_kmsRussell 2004 dissertation §3.8: 'Due to symmetry, the energy properties for inbound and outbound cyclers are identical.'
vinf_kms_at_encounters[1].vinf_kmsRussell 2004 dissertation §3.8 (same as above).
legs[0].tof_daysWikipedia / McConaghy 2002: symmetric 146-day fast transit.
period.yearsEarth-Mars synodic 2.135 yr — spec.md §9.