Iodine thruster
WebIodine Satellite (iSat) is a technology demonstration satellite of the CubeSat format that will undergo high changes in velocity [quantify] from a primary propulsion system by using a Hall thruster with iodine as the propellant. The spacecraft will also perform changes of its orbital altitude, and demonstrate deorbit capabilities to reduce space junk. WebWith a dry mass of 280 g and a volume of 180 cm3, the iodine μACFT EM is designed to fit inside of the tuna can extension of the 3U+ CubeSat structure. This form factor makes it incredibly small relative to other iodine thrusters. The measured thrust of the iodine μACFT is 227 - 254 μN, with a total system power consumption of 8.3 - 11.6 W.
Iodine thruster
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Web22 jan. 2024 · ThrustMe launched its iodine thruster on a commercial research nanosat called SpaceTy Beihangkongshi-1 that went into space in November 2024. It was test fired earlier this month before being used to change the orbit of the satellite. Published 22 January 2024 Last updated at 26 January 2024 - 09:43 WebIodine propellant for ion thrusters offers significant improvements in volume/space efficiency over xenon propellant systems presently in use today. The propellant can be stored in its solid state at very low pressure, whereas xenon must be stored in a compressed gas state at high pressure requiring additional tankage structure to contain the gas.
Web30 mrt. 2016 · Most state-of-the-art electric space propulsion systems such as gridded and Hall effect thrusters use xenon as the propellant gas. However, xenon is very rare, expensive to produce, and used in a number of competing industrial applications. Alternatives to xenon are currently being investigated, and iodine has emerged as a … WebFor the very first time, an Iodine-fueled ion thruster has been demonstrated in-orbit. Developed by ThrustMe in France, this technology is more efficient and…
Web30 mrt. 2016 · The thruster efficiency is however slightly higher for iodine compared with xenon, due to its lower ionization potential. This demonstrates that iodine could be a viable alternative propellant for gridded plasma thrusters. ACKNOWLEDGMENTS Atomic and molecular data obtained on demand and calculated by James Hamilton and Professor … WebIodine is an alternative to the state-of-the-art propellant xenon. Compared to xenon, iodine stores as a solid at much higher density and at a much lower pressure. Because iodine …
Web6 aug. 2024 · Moreover, iodine can easily be bound by a cryopump in terrestrial tests of thrusters, temperatures of ≈180 K are cold enough for yielding a sticking coefficient close to 1. Therefore, cryopumping can be realized cheaply …
Web1 jan. 2024 · Iodine as an ideal gas is considered as the propellant. The electric potential method with DC discharge is taken because of the nature of HET. A fluid model of plasma is taken hence, the velocity distribution of each species is not accounted. Partially ionized gases are not taken into consideration. Titanium is considered as the thruster material. swordfish 40908Web8 apr. 2024 · Phase Four announced April 8 it received a $750,000 Phase 2 Small Business Innovation Research (SBIR) award from the U.S. Air Force’s AFWERX program to test using iodine as a propellant in the... texline associatesWebThrustMe’s I2T5 is a non-pressurized cold gas propulsion system operating with solid iodine propellant. The I2T5 stand-alone system includes the propellant storage, flow control, … swordfish69 manafortWeb16 jan. 2024 · Two sets of performance data of the same radio-frequency ion-thruster (RIT) have been recorded using iodine and xenon, respectively, as propellant. To characterize the thruster’s performance, we have recorded the radio-frequency DC-power, required for yielding preset values of the extracted ion-beam currents, as a function of mass flow. swordfish 800xc 8 sheet cross-cut shredderWeb13 Iodine Feed System: BHT-200-I. • A laboratory iodine propellant feed was designed, fabricated, and assembled at NASA GRC. • VACCO iodine compatible PFCV was integrated with iodine feed system. • Iodine feed system allows for option to operate the thruster with xenon or iodine propellant. swordfish a3 guillotineWeb1 apr. 2024 · We have investigated the feasibility of a HET using in-situ water electrolysis by experimentally measuring the performance of a laboratory prototype that was designed to operate on oxygen as a propellant. The thruster was operated on powers ranging from 492 W to 2880 W, and mass flow rates of oxygen ranging from 0.985 mg −1 to 1.85 mg −1. tex lilithWeb29 mei 2024 · Abstract. The performance of an iodine radio ion thruster with a 4 cm diameter (IRIT4) was studied experimentally in this paper. Regulation of the mass flow … swordfish 2 movie