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Hybrid propulsion systems for space exploration missions

D. Darooka

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Abstract

Combinations of nuclear thermal propulsion (NTP), nuclear electric propulsion (NEP), and chemical propulsion are discussed. Technical details are given in viewgraph form. The characteristics of each configuration are discussed, particularly thrust characteristics.

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Combinations of nuclear thermal propulsion (NTP), nuclear electric propulsion (NEP), and chemical propulsion are discussed. Technical details are given in viewgraph form. The characteristics of each configuration are discussed, particularly thrust characteristics.

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Available abstract

Combinations of nuclear thermal propulsion (NTP), nuclear electric propulsion (NEP), and chemical propulsion are discussed. Technical details are given in viewgraph form. The characteristics of each configuration are discussed, particularly thrust characteristics.

Key concepts: Propulsion, In-space propulsion technologies, Thrust, Electrically powered spacecraft propulsion, Aerospace engineering, Spacecraft propulsion, Space (punctuation), Engineering

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