Fig. 3. (A) The hot-fire test diagram of the thruster and (B) the thermal decomposition and combustion processes of the ammonium dinitramide (ADN)-based propellant within the thruster. (IMAGE)

Beijing Institute of Technology Press Co., Ltd

Fig. 3. (A) The hot-fire test diagram of the thruster and (B) the thermal decomposition and combustion processes of the ammonium dinitramide (ADN)-based propellant within the thruster.

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Fig. 3. (A) The hot-fire test diagram of the thruster and (B) the thermal decomposition and combustion processes of the ammonium dinitramide (ADN)-based propellant within the thruster.

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Space: Science & Technology

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