Falcon Dragon Crew Mission Planner & Trajectory Calculator

1. Mission Configuration CCtCap Spec Active

Target CCtCap Designation

Dragon Payload & Crew Mass 12,500 kg

Min: 11,500 kg Max: 13,800 kg

Launch Azimuth (θ) 42.5°

Target ISS Inc: 51.6° (Cape Canaveral SLC-40 / LC-39A)

B1-Stage Landing Fuel Reserve 8.4%

Minimum recovery threshold: 6.0%

Booster Recovery Vessel ASOG

Insertion Orbit Target

Deterministic verification & telemetry exports supported

Total Orbit ΔV 9,350 m/s Nominal required: 9,280 m/s

Booster Recovery Margin 11.2% Droneship downrange: 540 km

ISS Docking Phase 26.5 hrs Free-return reserve: >72h

Mission Feasibility MISSION PROFILE FEASIBLE NASA Safety Factor: 1.34

T+ 00:02:40 • MECO & STAGE SEPARATION

Flight Phasing & Free-Return Milestones Profile: Crew-15 / LC-39A

T+ 00:00:00 Liftoff SLC-40 / LC-39A Florida

T+ 00:02:28 MECO & Separation Alt: 67 km • Mach 5.9

T+ 00:08:35 Booster Landing ASOG Droneship

T+ 00:08:48 SECO-1 / Orbit 210 x 390 km Insertion

T+ 00:12:00 Dragon Separation Nosecone open • Draco active

T+ 26:30:00 ISS Soft Docking Harmony Forward / Zenith

CCtCap Flight Plan: Crew-15 with payload 12,500 kg achieving total ΔV of 9350 m/s. First-stage booster recovery via ASOG yields landing fuel margin of 11.2%. Phased rendezvous to ISS (400km x 400km, 51.6°) completes docking in 26.5 hours. Status: MISSION PROFILE FEASIBLE.