A combined launch vehicle and satellite system
US-2024051685-A1 · Feb 15, 2024 · US
US9963250B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9963250-B2 |
| Application number | US-201214346098-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 20, 2012 |
| Priority date | Sep 20, 2011 |
| Publication date | May 8, 2018 |
| Grant date | May 8, 2018 |
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Official abstract text for this publication.
This invention relates to a propulsion bay to be transported, at least temporarily, in a space launch vehicle and comprising an adapter that co-operates with at least one system located, at least temporarily, on board the bay, said system comprising an electrical power supply. The bay is characterized in that it also comprises at least one electric space propulsion engine that can be powered by the power supply of the system.
Opening claim text (preview).
The invention claimed is: 1. A propulsion bay configured to be transported at least temporarily in a space launch vehicle, comprising: an adapter which cooperates with at least one of a first, a second, or a third system loaded temporarily on the propulsion bay, said first, second, and third systems being removably engageable with said adapter, the adapter comprising a carrier structure having a substantially cylindrical shape and an inner space to receive the first system loaded in the carrier structure, the carrier structure comprising an end to cooperate with the second system, the adapter being adapted to cooperate with the third system forming an additional liquid or solid space propulsion system, each of the first, second, and third systems comprising an electric power supply; and at least one electric space propulsion engine adapted to be powered by the power supply of any of the first, second and third systems. 2. The bay according to claim 1 , wherein the first system and/or the second system form artificial satellites configured to orbit in space. 3. The bay according to claim 2 , wherein the carrier structure has openings adapted for deployment of solar panels of the power supply of the first system forming an artificial satellite, via the openings.
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