Concepedia

Concept

in-space propulsion systems

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41.8K

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3.2K

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606

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Next-Generation Xenon Propulsion

1998 - 2006

The period witnessed maturation of high-power xenon ion propulsion, tracing NSTAR heritage to NEXT with scalable thruster architectures, extended-life testing, and mission-ready integration across deep-space programs. Strategic programmatic framing and planning for electric propulsion emerged, emphasizing mission architectures and cross-mission benefits that guided SEP and NEXT choices. Hall thruster evaluations and rigorous testing of propulsion hardware, including environmental qualification and endurance studies, became central to establishing reliable, flight-ready systems.

Evolution and maturation of high-power ion propulsion, tracing NSTAR heritage to NEXT, with scalable thruster architectures, extended life testing, and mission-ready integration across NASA's deep-space programs [2], [1], [3], [7], [10], [9], [15], [18].

Programmatic framing and strategic planning for electric propulsion within NASA, highlighting program directions, mission architectures, and cross-mission benefits driving SEP and NEXT choices [5], [13], [6], [16], [19].

Hall thruster-focused evaluation for deep-space missions, including performance analyses, configuration tradeoffs, and trajectory implications of using Hall-type electric propulsion [17], [14], [16].

Testing, environmental qualification, and endurance studies of electric propulsion hardware, including NSTAR/NSTAR thrusters, thermal testing, and microthruster endurance experiments [15], [9], [11], [20].

Mission concept studies assessing NEXT/SEP role in deep-space exploration and Mars missions, comparing electric propulsion-enabled scenarios with chemical baselines and mapping candidate mission sets [10], [6], [16], [8].

High-Power Electric Propulsion Maturation

2007 - 2013

Integrated Electric Propulsion Convergence

2014 - 2020