Russell-Ocampo cycler 5.66Gfh3 (3-synodic ballistic with 2:1 resonant orbit)

russell-ch4-5.66Gfh3 · source: literature · validation: V0

Signature

Bodies: E-M
Primary: Sun (default — heliocentric)
Sequence (canonical): E-E-E-M-M
Sense: outbound
Orbit class: Cycler
strict cycler (infinite returns)
Cycler class: multi-arc
Trajectory regime: ballistic
Maintenance ΔV band: unclassified
Model assumption: circular-coplanar
Idealised: planets on circles, coplanar ecliptic.
Period: 6.410 yr (3 × E-M synodic)
Maintenance ΔV: 0 km/s — strict ballistic
Priority date: 2003-02-09

V∞ at encounters

E (encounter 1): 5.66 km/s
Russell 2004 Table 4.11 row 5392 et seq.: v_inf E = 5.66 km/s. This cycler family dominates Table 4.11 with ~30 minor variants differing only in trailing leg arguments.
M (encounter 2): 9.26 km/s
Russell 2004 Table 4.11: v_inf M = 9.26 km/s.

Cycle-level identity (multi-arc invariants)

Aphelion ratio (AR): —
Turn ratio (TR): 1.26
Transit times (days): 113 d, 113 d

Russell 2004 Table 4.11: aphel = 2.17 AU. Uses 2:1 resonant full-rev return per dissertation line 5526.

Orbit view 2.5D ecliptic projection

spacecraft: idealized coplanar ellipse planets: J2000 osculating ellipse (Standish & Williams Table 1) orientation: coplanar-idealized (no Ω/ω published — in-plane ellipse)

3D view not available for multi-arc trajectories yet. The 3D system can now render a numerically-sampled polyline (n-body or multi-arc), but no sampled trajectory is published for this row — each leg is a separate ellipse with honest gaps where elements are unpublished (the 2D view above shows them). The button will appear here once a sampled path is exported for this trajectory; we never interpolate one from the catalogue's per-leg (a, e).

— — planet orbit (true J2000 ellipse) ◌ max aphelion ring (sourced)

Not-published gaps (never interpolated):

E → M — segment elements (a, e) not published; no curve drawn.
M → E — segment elements (a, e) not published; no curve drawn.
E → E — segment elements (a, e) not published; no curve drawn.
E → E — segment elements (a, e) not published; no curve drawn.

Real DE440 encounter dates (3)

2031-03-09 V∞ 5.86 / 9.66 km/s
2033-04-07 V∞ 4.58 / 9.86 km/s
2035-06-06 V∞ 5.83 / 8.72 km/s

Real, verifiable JPL DE440 geometric-match dates (see Launch windows). Positions on the map are idealized; these are the true dates.

Legs (trajectory segments)

E → M: 113 d, 0 revs
Russell 2004 Table 4.11: t_out = 113 days.
M → E: 113 d, 0 revs
Russell 2004 Table 4.11: t_in = 113 days.
E → E: (TOF not published)
Intermediate Earth-Earth loop 1 of 2 for this 3-synodic cycler (sequence E-E-E-M-M); fills part of the 6.41-yr period between Mars encounters. Multi-rev arc — tof_days / n_revs / branch / (a,e) to be set by the multi-rev Lambert solver.
E → E: (TOF not published)
Intermediate Earth-Earth loop 2 of 2 for this 3-synodic cycler (sequence E-E-E-M-M); fills part of the 6.41-yr period between Mars encounters. Multi-rev arc — tof_days / n_revs / branch / (a,e) to be set by the multi-rev Lambert solver.

Definition status

incomplete — core fields missing or known-unknowns tracked below

Family: Russell 3-synodic Earth-Mars ballistic · Russell-Ocampo cycler code

Known-unknowns (3)

Values we expect to exist but have not yet filled (distinct from "not applicable"). Tracked per upstream docs/spec.md §16.6.4.

trajectory.segments[loop-ee-*] [derive]
The 2 intermediate Earth-Earth loop arc(s) tof_days / n_revs / branch / (a,e) are computable once the multi-rev Lambert solver closes the arc(s) to the published 5.66/9.26 km/s V-infinity; not yet derived. Russell 2004 tabulates only t_out/t_in + the aggregate aphelion, not the loop arc(s).

source: multi-rev Lambert solver; Russell 2004 Table 4.x leg descriptors
trajectory.segments[out-em].a_au [unknown]
Per-segment (a,e) of the outbound generic-return arc not tabulated by Russell 2004 (orbit_elements.a_au/e are null for the same reason — each generic-return arc has its own (a,e); only the aggregate aphelion is well-defined).

source: Russell 2004 dissertation Table 4.x leg descriptors g(...)/G(...)
trajectory.segments[ret-me].a_au [unknown]
Per-segment (a,e) of the return generic-return arc not tabulated by Russell 2004; same source gap as out-em.

source: Russell 2004 dissertation Table 4.x leg descriptors g(...)/G(...)

Primary citation

Russell, R. P. & Ocampo, C. A. (2003). Global Search and Optimization for Free-Return Earth-Mars Cyclers. AAS Paper 03-145.

orbit source Russell 2004, Tables 4.9 / 4.13 orbit fidelity circular-coplanar V∞ source Russell 2004, Tables 4.9 / 4.13 V∞ fidelity circular-coplanar

Corroborating sources

Russell, R. P. (2004). Global Search and Optimization for Free-Return Earth-Mars Cyclers. PhD dissertation, UT Austin. · link
Dissertation line 5526-5527: 'Cycler 5.66Gfh uses a 2:1 resonant orbit, and also has short transit times and even better turning angles.' TR = 1.26 (best variant).

Notes

Russell calls out the 5.66xxx family as "consistently low ΔV requirements for all launch windows" — dissertation line 7420 notes "Several three-synodic period cyclers, such as those with the prefix 5.658 as seen in Figure 5.6, also exhibit relatively flat lines that hover near a ΔV of zero." (The 5.658 prefix in Figure 5.6 corresponds to the 5.66xxx parent cyclers when grouped by the realistic-ephemeris simple-model V_inf.) The 5.658Gfh+ff3 parent cycler no. 162 has the lowest realistic-ephemeris average ΔV in Table 5.6 at 24 m/s. Many rows in Table 4.11 share these (V_inf, ToF, aphel) values differing only in the trailing leg arguments (Russell calls these "subtle differences" at line 5494). Cataloguing one canonical member captures the family signature.

Source quotes (per-field provenance)

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

delta_v_kms: Derived from Russell 2004's tabulated AR / TR via the M2 powered-flyby surrogate (src/cyclerfinder/core/flyby.py): ΔV ≈ (V∞_E + V∞_M) × max(0, 1 − TR) + (1 − AR) × (V∞_E + V∞_M) × 0.025 [AR-correction term active only when AR < 1]. Upper bound; biases near-ballistic entries toward 'requires nudge'. Strict-ballistic rows (AR ≥ 1 AND TR ≥ 1) give ΔV = 0 exactly. AR/TR primary values: Russell 2004 Table 4.11 (5.66Gfh row, first variant): aphel=2.17 AU, TR=1.26, v∞E=5.66, v∞M=9.26.
vinf_kms_at_encounters[0].vinf_kms: Russell 2004 Table 4.11 row 5392+: v_inf E = 5.66.
vinf_kms_at_encounters[1].vinf_kms: Russell 2004 Table 4.11: v_inf M = 9.26.
legs[0].tof_days: Russell 2004 Table 4.11: t_out = 113.
orbit_elements.aphelion_au: Russell 2004 Table 4.11: aphel = 2.17 AU.