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Boeing did not license the technology and communication stopped. [46] In 2012, a Boeing representative confirmed that Boeing Phantom Works used to explore exotic forms of space propulsion, including Shawyer's drive, but such work later ceased. They confirmed that "Phantom Works is not working with Mr. Shawyer," nor pursuing those explorations.
These propulsion technologies are intended to provide effective exploration of the Solar System and may permit mission designers to plan missions to "fly anytime, anywhere, and complete a host of science objectives at the destinations" and with greater reliability and safety. With a wide range of possible missions and candidate propulsion ...
Exolaunch was a spin-off from Technische Universität Berlin. [1] [2] Since its founding, Exolaunch has supported the deployment of over 100 satellites. [3]Exolaunch has provided mission management and launch services for payloads on Soyuz and Electron rockets [4] and has announced agreements with SpaceX and New Space India Limited.
A reactionless drive is a hypothetical device producing motion without the exhaust of a propellant.A propellantless drive is not necessarily reactionless when it constitutes an open system interacting with external fields; but a reactionless drive is a particular case of a propellantless drive that is a closed system, presumably in contradiction with the law of conservation of momentum.
Launch of Electron in start of the "Birds of a Feather" mission. Electron is a two-stage small-lift launch vehicle built and operated by Rocket Lab.The rocket has been launched to orbit 55 times with 51 successes and four failures.
Test-firing of the Psyche spacecraft's SPT-140 at the Jet Propulsion Laboratory.. SPT-140 is a solar-powered Hall-effect ion thruster, part of the SPT-family of thrusters.SPT stands for Stationary Plasma Thruster.
The NEXT thruster has demonstrated, in ground tests, a total impulse of 17 MN·s; which as of 2010 was the highest total impulse ever demonstrated by an ion thruster. [2] A beam extraction area 1.6 times that of NSTAR allows higher thruster input power while maintaining low voltages and ion current densities, thus maintaining thruster longevity.
Selected advanced electric propulsion projects developed propulsion technology systems in the 50 to 300 kilowatts (67 to 402 hp) range to meet the needs of a variety of deep space mission concepts. The three NextSTEP advanced propulsion projects, $400,000 to $3.5 million per year per award, were limited to a three-year performance period ...