An inflation assembly for an evacuation system may comprise a manifold defining an interior volume and a plurality of inflators fluidly coupled to the manifold. Each inflator of the plurality of inflators may include a solid gas generating material and an igniter configured to ignite in response to receiving an ignite signal. The solid gas generating material may be configured to generate a gas in response to an ignition of the igniter.

Propulsion systems that generate thrust from pressure generated by thermally decomposing a chemical blowing agent (CBA). In some embodiments, the CBA decomposes exothermically such that once thermal decomposition has been initiated, the thermal decomposition continues without additional energy input. In some embodiments, the CBA is utilized in a digital-microthruster array containing microthrusters that can be individually activated to provide thrust. In some embodiments, a CBA may be stored in one or more CBA-storage chambers that can be individually activated to charge and/or recharge a pressure tank that stores gas from the CBA decomposition under pressure for providing thrust. These and other embodiments are disclosed. Such propulsion systems can be used for any of a variety of spacecraft, including micro- and nano-satellites. Corresponding methods of generating thrust are also disclosed.

The present invention relates generally in gaseous oxygen propulsion systems with solid-phase chemical oxygen generation for in-space propulsion systems. Chemical oxygen generation is provided by alkali metal chlorates, alkali metal perchlorates or metal peroxides.

The present invention relates generally in gaseous oxygen propulsion systems with solid-phase chemical oxygen generation for in-space propulsion systems. Chemical oxygen generation is provided by alkali metal chlorates, alkali metal perchlorates or metal peroxides.

The present application belongs to the field of compounds, and particularly relates to the perovskite-type compound ABX.sub.3. As a finding of the present application, the structural characteristics of the perovskite type enables the type of compound to be highly stable, thus overcoming the unsafety of an explosive having poor stability in the prior art. Meanwhile, the structural characteristics of the compound, such as rich energetic ligands, as well as the alternately arranged oxidizing energetic anions and reducing organic cations in the space, endow the compound with excellent performance on instantaneously releasing energy at detonation. The resulting three-dimensional structure allows the compound to not only have an energetic material effect but also overcome shortcomings of some existing energetic materials.

The present application belongs to the field of compounds, and particularly relates to the perovskite-type compound ABX.sub.3. As a finding of the present application, the structural characteristics of the perovskite type enables the type of compound to be highly stable, thus overcoming the unsafety of an explosive having poor stability in the prior art. Meanwhile, the structural characteristics of the compound, such as rich energetic ligands, as well as the alternately arranged oxidizing energetic anions and reducing organic cations in the space, endow the compound with excellent performance on instantaneously releasing energy at detonation. The resulting three-dimensional structure allows the compound to not only have an energetic material effect but also overcome shortcomings of some existing energetic materials.

An inflation system for an evacuation system may comprise an inflator and a controller operationally coupled to the inflator. The inflator may include a solid gas generating material and an igniter configured to ignite in response to receiving an ignite signal. The solid gas generating material may be configured to generate a gas in response to an ignition of the igniter. The controller may be configured to send the ignite signal to the inflator.

An inflation system for an evacuation system may comprise an inflator and a controller operationally coupled to the inflator. The inflator may include a solid gas generating material and an igniter configured to ignite in response to receiving an ignite signal. The solid gas generating material may be configured to generate a gas in response to an ignition of the igniter. The controller may be configured to send the ignite signal to the inflator.

Devices for generating a desired gas or mixture of gases by thermally decomposing a polymer, and methods of making and using such devices, are provided. The resulting gas or mixture of gases, or a fraction thereof, can be used for any suitable purpose, including but not limited to use as an inflating or lifting gas. The devices and methods of the disclosure provide greater mass and volumetric efficiency for gas generation and storage relative to conventional gas generation solutions and are safer and simpler than compressed gas cylinders or liquefied gas storage.

An inflation system is disclosed. In various embodiments, the inflation system includes a solid-propellant gas generator; and a gas motor having a turbine coupled to the solid-propellant gas generator and a compressor configured for coupling to an inflatable device.