Abstract: In a method of facilitating flight operations, a payload is coupled to a spacecraft via a payload interface. The relative alignment of the payload and the spacecraft is dynamically adjusted (e.g., for thrust alignment) while the payload remains coupled to the spacecraft.

Abstract: A method at an electronic device with a display includes: displaying a user interface having a first region and a second region; receiving, and displaying in the first region of the user interface, a live video stream of a physical environment captured by a remote video camera; displaying, in the second region, a timeline corresponding to a timespan for a first portion of a duration during which the live video stream may have been recorded; in response to receiving a user interaction to move the timespan to a second portion of the duration, transitioning the displayed timeline to a new timeline that corresponds to the timespan for the second portion, and while transitioning, displaying, in the first region, a subset of video frames representing the first and/or second portion of the duration.

Abstract: The present disclosure provides systems and methods for propulsion. The system may comprise one or more motor assemblies for driving at least one shaft or rotor of a vehicle. The motor assemblies may comprise one or more motor windings and/or magnets. The system may comprise one or more fuel cells in fluid communication with the motor assemblies. The fuel cells may be configured to generate electrical energy from a fuel that is directed through a portion of the motor assemblies to (i) cool the motor windings and the magnets and (ii) and heat the fuel before the fuel enters the fuel cells. The system may comprise a combustion chamber in fluid communication with the fuel cells. The combustion chamber may be configured to combust an exhaust flow from the fuel cells to (i) react unused hydrogen exhausted from the fuel cells and (ii) provide thermal and/or mechanical power.

Abstract: In a method of facilitating flight operations, a payload is coupled to a spacecraft via a payload interface. The relative alignment of the payload and the spacecraft is dynamically adjusted (e.g., for thrust alignment) while the payload remains coupled to the spacecraft.

Abstract: A spacecraft structure for transporting propellant to be consumed by a thruster includes storing the propellant in the spacecraft in a solid state during at least a portion of a take-off procedure and supplying the propellant to the thruster in a liquid or vaporous state when the spacecraft is in space.

Abstract: A method in a spacecraft for transporting propellant to be consumed by a thruster includes storing the propellant in the spacecraft in a solid state during at least a portion of a take-off procedure and supplying the propellant to the thruster in a liquid or vaporous state when the spacecraft is in space.