SPT-100 is a Hall-effect ion thruster, part of the SPT-family of thrusters. SPT stands for Stationary Plasma Thruster. It creates a stream of electrically charged xenon ions accelerated by an electric field and confined by a magnetic field.[1]
The thruster is manufactured by Russian OKB Fakel, and was first launched onboard the Gals-1 satellite in 1994.[2] In 2003, Fakel debuted a second generation of the thruster, called SPT-100B, and in 2011, it presented further upgrades in SPT-100M prototypes.[3] As of 2011, SPT-100 thrusters were used in 18 Russian and 14 foreign spacecraft, including IPSTAR-II, Telstar-8, and Ekspress A and AM constellations.[3]
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Transcription
Specifications
| Parameter | SPT-100 | SPT-100B | SPT-100M | SPT-100D |
|---|---|---|---|---|
| Power (W) | 1350 | 1350 | 1350 | 2500 |
| Thrust (mN) | 80 | 83 | 90.2 | 112 |
| Thrust-to-power level (mN/kW) | 59.26 | 61.48 | 66.81 | 44.80 |
| Specific impulse (s) | 1,600 | 1,600 | 1,734 | 2,200 |
| Efficiency (%) | 50 | |||
| Voltage (V) | 300 | 300 | 600 | |
| Discharge current (A) | 4.5 | 4.5 | 4.17 | |
| Mass (kg) | 4 | 4.7 | ||
| Reference: [4]: 14 [3]: 4 [5]: 6 | ||||
See also
References
- ^ Sankovic, John M.; Hamley, John A.; Haag, Thomas W. (1993). "Performance Evaluation of the Russian SPT-100 Thruster at NASA LeRC" (PDF). EP-PC-93-094. Retrieved 26 January 2017.
- ^ "ОКБ ФАКЕЛ / About". Archived from the original on 6 February 2017. Retrieved 26 January 2017.
In the early 80s, EDB Fakel started its serial production of the thruster types SPT-50, SPT-60, and SPT-70. The first satellite equipped with SPT-70, Geizer 1, was launched in 1982; and in 1994, a new SPT-100 model was implemented aboard the communication satellite, Gals-1
- ^ a b c Mitrofanova, O. A.; Gnizdor, R. Yu.; Murashko, V. M.; Koryakin, A. I.; Nesterenko, A. N. (2011). "New Generation of SPT-100" (PDF). IEPC-2011-041. Retrieved 26 January 2017.
- ^ Brophy, John R. (15 March 1992). "Stationary plasma thruster evaluation in Russia" (PDF). 19930016017. Retrieved 26 January 2017.
- ^ Gnizdor; Komarov; Mitrofanova; Saevets; Semenenko. High-impulse SPT-100D thruster with discharge power of 1.0...3.0 kW (PDF). 35th International Electric Propulsion Conference. IEPC-2017-40. Retrieved 9 March 2019.
External links
This page was last edited on 26 March 2024, at 23:34