Electrically powered spacecraft/airship
First Claim
Patent Images
1. An spacecraft/airship comprising:
- (a) one or more gas retaining structures;
(b) a spacecraft body connected to one or more gas retaining structures;
(c) one or more lifting gasses;
(d) one or more electrically powered thrusters;
(e) means for supplying a lifting gas from one or more gas retaining structures to said one or more electrically powered thrusters; and
(f) a means of supplying electric power to said one or more electrically powered thrusters.
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Abstract
An spacecraft/airship, which uses buoyancy and thrusters to ascend into space with lifting gas as propellant or fuel for thrusters, which may be conventional thrusters or electric turbojets or ion thrusters. The airship aspect has gas retaining structures that can regulate the density of the gasses within. The spacecraft aspect provides for mounting thrusters, control, power, services, and interior space for missions of the spacecraft/airship.
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Citations
22 Claims
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1. An spacecraft/airship comprising:
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(a) one or more gas retaining structures;
(b) a spacecraft body connected to one or more gas retaining structures;
(c) one or more lifting gasses;
(d) one or more electrically powered thrusters;
(e) means for supplying a lifting gas from one or more gas retaining structures to said one or more electrically powered thrusters; and
(f) a means of supplying electric power to said one or more electrically powered thrusters. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15)
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16. A system for sub-orbital, orbital, and extra-orbital space flight from a planetary surface with a combination airship and spacecraft, comprising:
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(a) an airship means;
(b) a spacecraft means;
(c) means for regulating the buoyancy of the combination airship and spacecraft to control the ascent of the combination airship and spacecraft as an airship;
(d) electric thruster means for creating upward thrust on the combination airship and spacecraft during the ascent of the combination airship and spacecraft;
(e) means for receiving beamed microwave energy for supplying the combination airship and spacecraft with electric power; and
(f) means for beaming microwave energy to the combination airship and spacecraft;
so that the ascent of the combination airship and spacecraft into space is initiated with upward thrust from buoyancy of the combination airship and spacecraft when the planetary atmosphere is sufficiently dense to provide buoyancy, and then continued into space by the activation and operation of thrusters.- View Dependent Claims (17, 18, 19, 20, 21)
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22. An spacecraft/airship comprising:
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(a) one or more gas retaining structures;
(b) a spacecraft body connected to one or more gas retaining structures;
(c) one or more lifting gasses;
(d) one or more electrically powered thrusters;
(e) means for supplying a lifting gas from one or more gas retaining structures to said one or more electrically powered thrusters;
(f) means for receiving beamed microwave energy for supplying the combination airship and spacecraft with electric power; and
(g) means for beaming microwave energy to the combination airship and spacecraft.
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Specification