Robotic ISS airlock deployment expands external payload capacity using CBM and FRAM interfaces while reducing EVA and crew time.
Segmented hollow box substructures with dynamic dagger pins resolve the contradiction between structural integrity and maintenance downtime.
A maneuverable cowl element extends around a rocket nozzle to mask the exhaust during atmospheric flight.
Maneuverable flaps maximize drag to reduce speed while minimizing structural loads and heating on the crew compartment.
Wing lift in the atmosphere changes the orbital plane, reducing fuel consumption compared to perpendicular engine firing.
A reusable launch vehicle system monitors position and uses aerodynamic control surfaces to adjust flight paths during ascent.