Transfer Orbit

HOHMANN TRANSFER

INTERPLANETARY TRAJECTORY LAB

CENTRAL BODY

INITIAL RADIUS (r₁ - KM)

FINAL RADIUS (r₂ - KM)

TOTAL Delta V REQUIRED

0.000

KM/S

Burn 1: 0.000 km/s

Burn 2: 0.000 km/s

TRANSFER TIME:

0.00

HOURS

Hohmann ΔV

Efficiency Over Speed. The Hohmann transfer is the Low-Energy Path. It uses the planet's gravity to do the heavy lifting, requiring only two short "kicks" of thrust to change worlds.

🏁 Departure: Burn 1 creates the ellipse.
📍 Arrival: Burn 2 circularizes the orbit.
⛽ Fuel: The most "bang for your buck" maneuver.

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TRANSFER SEQUENCE

ΔV-1 COMPLETE

APOAPSIS REACHED: ✅ 180°

HOHMANN-SYNC ACTIVE ✅

Logic: Δv

The Math of Survival. We calculate the Hohmann Transfer to find the Critical Minimum. In space, "More Power" usually means "More Weight," so we optimize for the curve.

⚖️ Mass Ratio: Keeping the rocket light enough to launch.
🕰️ Syncing: Matching the arrival with the planet's position.
🛑 Capture: Arriving slow enough to stay.

RESOURCE OPTIMIZER

FUEL: SAVE 45%

PATH: ✅ HOHMANN OPTIMAL

ECON-SYNC ACTIVE ✅

Hohmann Phasing

The Energy Bridge. It’s a game of Momentum Trading. We use a high-speed kick to buy altitude, then a second kick to pay for the "rent" of staying in the new neighborhood.

🏁 Perigee Kick: Increasing the semi-major axis of your orbit.
🛰️ Apogee Capture: Matching speeds with the target's height.
📉 Gravity Loss: Minimizing the time spent fighting the planet's pull.

ORBITAL PHASING

Δv: 3,900 m/s

ECCENTRICITY: ✅ 0.72

VECTOR-SYNC ACTIVE ✅

Mars-Hohmann

Interplanetary Timing. The Earth-Mars Hohmann transfer is a Nine-Month Coast. It turns the solar system into a giant clock where fuel efficiency dictates our arrival.

📅 26 Months: The wait time between launch windows.
🏎️ Delta-V: ~3.9 km/s needed to leave Earth's orbit.
🛑 Insertion: Slowing down to enter the Martian "Well."

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PHASE ALIGNMENT

∠ 44.3°

WINDOW: ✅ OPTIMAL LAUNCH

MARS-SYNC ACTIVE ✅