Space access system with reusable booster
A space access system may include a reusable booster limited to sub-orbital operation and having a fuselage. The reusable booster may include a tri-propellant propulsion system which may be configured to shift from a tri-propellant mode of operation to a bi-propellant mode of operation. The tri-prop...
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| Format: | Patent |
| Sprache: | eng |
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| Zusammenfassung: | A space access system may include a reusable booster limited to sub-orbital operation and having a fuselage. The reusable booster may include a tri-propellant propulsion system which may be configured to shift from a tri-propellant mode of operation to a bi-propellant mode of operation. The tri-propellant propulsion system may include at least one tri-propellant engine and at least one internal propellant tank mounted within the fuselage and being fluidly coupled to the tri-propellant engine. A payload may be mounted with the fuselage. The payload may have an upper stage. |
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