RFS Extraction — Rendezvous & Flight Simulator | Römer Industries
RFS EXTRACTION — RENDEZVOUS & FLIGHT SIMULATOR
3D orbital rendezvous · CW proximity ops · Hohmann transfer · Plotly 3D · /sims/rfs-extraction
ORB LW MAG PWR FLD RFS EMFF EMF ENTRY W1 W2 W3 W4 W5 W6 ACH LIB GMAT DASH
● LIVE /sims/rfs-extraction · Universal — callable by all workspaces & dataspaces · Römer Industries / EMASSC ·
RFS Extraction — Rendezvous & Flight Simulator
3D orbital rendezvous simulation · Hill-Clohessy-Wiltshire proximity ops · Hohmann/bi-elliptic transfer · Keplerian propagation with J2 perturbation
SI Units Universal Tool — W1–W6 Callable Plotly 3D Visualisation Animated Playback JetBrains Mono · Inter
ALTITUDE
400
km
ORBITAL VELOCITY
7.67
km/s
ΔV BUDGET
0.00
km/s
RANGE TO TARGET
—
km
INCLINATION
28.5
deg
ORBITAL PERIOD
92.1
min
PHASE ANGLE
0.0
deg
SIM TIME
T+00:00
hh:mm
⚙ ORBIT PARAMETERS
🚀 CHASER VEHICLE
🎯 RENDEZVOUS CONFIG
▶ PLAYBACK
10s
⚡ J2 PERTURBATIONS
⬡ ROUTE TO DATASPACE
T+00:00:00 SIM SPEED:
TRANSFER ΔV—
TRANSFER TIME—
PROPELLANT USED—
PHASE ANGLE REQ.—
INTERCEPT TIME—
CW RELATIVE MOTION
Compute orbit to generate CW proximity solution.
PARAMETERVALUEUNIT
TELEMETRY PARAMETER:
TIME (min)ALT (km)VEL (km/s)RANGE (km)ΔV (km/s)PHASE (°)
⚡ SWEEP CONFIGURATION
INPUTOUTPUT

⬡ JSON STATE

Full mission state — orbital elements, maneuver sequence, telemetry log, CW solution.

📊 CSV TRAJECTORY

Time-series trajectory data — altitude, velocity, range, ΔV, phase angle per time step.

🛰 GMAT SCRIPT

GMAT mission script for /data/w5 — propagator, maneuver nodes, relative motion solver.

📄 TXT MANIFEST

Human-readable mission manifest — parameters, results summary, CW solution, burn schedule.

🖼 PNG SNAPSHOT

Export the current 3D orbital view as a high-resolution PNG image.

📋 YAML CONFIG

YAML configuration — all parameters for reproducible mission runs and pipeline integration.