NEW SHEPARD LANDING PROTOCOL
Mission: NS-16 │ Date: 2021-07-20 │ Crew: Jeff Bezos, Mark Bezos, Wally Funk, Oliver Daemen
Status: Perfect vertical descent. Zero horizontal deviation. Touchdown velocity: 0 m/s.
Mission: NS-16 │ Date: 2021-07-20 │ Crew: Jeff Bezos, Mark Bezos, Wally Funk, Oliver Daemen
Status: Perfect vertical descent. Zero horizontal deviation. Touchdown velocity: 0 m/s.
The Short North grid teaches us: every camera angle is a constraint. On New Shepard, the BE-3PM engine throttles to 11% thrust at 10km altitude, holding hover until the final burn. This is not poetry—it is the difference between a crater and a pad.
| Phase | Altitude | Thrust % | Δv Budget | Constraint |
|---|---|---|---|---|
| Tailcone Separation | 105 km | 0% | N/A | Apogee confirmation |
| Retro Burn Initiation | 10 km | 100% → 11% | 120 m/s | Engine gimbal lock |
| Hover Hold | 100 m | 11% | 0 m/s | GPS/INS fusion |
| Final Descent | 0 m | 11% → 0% | -0.3 m/s² | Pad contact sensors |
Location: West Texas, USA │ Coordinates: 30.6° N, 104.5° W
The landing zone is not chosen by luck. It is calculated against wind shear profiles, dust particulate density, and thermal gradients that mirror our own Red Horizon simulations. When the booster touches down, the regolith displacement must not exceed 3mm—any more and the next ascent risks structural fatigue.
This is the same discipline we apply to the Scar Festival welds: measure the gap, calculate the stress, execute the pass. No margin for error.
While the booster lands vertically, the crew capsule deploys three main parachutes at 2.5km altitude. Each chute bears 4,200 kg of load. The canopy inflation pressure must stabilize within 0.8 seconds—or the capsule tears.
Protocol:
Le Guin wrote that survival is not a miracle—it is a procedure followed correctly. NS-16 proves this.
This landing sequence informs our own dome construction: