Odyssey — Void Orbital

Mission Plan

Patched-conic trajectory design

Origin

Target

Mission heritage & notes

Park alt · origin (km)

Park alt · target (km)

Launch from surface (incl. est. losses)

Launch latitude (°) · rotation credit Blank gives no rotation credit. A latitude credits the surface speed of a launch toward the body's rotation.

Land on target

Capture orbit eccentricity e 0 captures into the circular parking orbit; above 0 into an ellipse whose periapsis is the target parking altitude. Not used when landing.

Include plane-change (Δi) cost

Asteroids & comets ◆ ◆ ◆ ☄ Zoom to mission system

Δv Ledger

Configure the mission and compute. Grounded in Prussing & Conway, Orbital Mechanics — vis-viva, patched conics, Lambert by Izzo's method (2015).

Telemetry

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Click a body or use the menus

Vehicle · Tsiolkovsky

Input mode

Wet mass (t)

Dry mass (t)

Specific impulse (s)

Electric thrust

Unit

● main belt 2.1–3.3 AU · ● Kuiper belt 30–50 AU
drag rotate · scroll/pinch zoom · click a body to fly to it
distances compressed: ∝ r^0.55 about the Sun · orbits show e & i
◆ asteroid · ◆ ◆ ringed: mining target (metal / water) · comets: coma, tails, trail