Vacuum test of a micro-solid propellant rocket array thruster
نویسندگان
چکیده
منابع مشابه
Improvement of Micro Solid Rocket Array Thruster for Reliable Operation in Vacuum
We are developing a micro solid propellant rocket array thruster for simple attitude control of a 10 kg class micro spacecraft. To improve the contact between the ignition heater and the ignition charge of lead thiocyanate / potassium chlorate (RK), the loading method of RK was improved. Ignition probability increased to 100 % in air and 83 % in vacuum. When the pellet diameter of boron / potas...
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ژورنال
عنوان ژورنال: IEICE Electronics Express
سال: 2004
ISSN: 1349-2543
DOI: 10.1587/elex.1.222