SPT-100

{{Short description|Hall-effect ion thruster}}

Image:Russian stationary plasma thrusters.jpg

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.{{cite web|url=https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19940019157.pdf|title=Performance Evaluation of the Russian SPT-100 Thruster at NASA LeRC|format=PDF|first1=John M.|last1=Sankovic|first2=John A.|last2=Hamley|first3=Thomas W.|last3=Haag|year=1993|id=EP-PC-93-094|accessdate=26 January 2017}}

The thruster is manufactured by Russian OKB Fakel, and was first launched onboard the Gals-1 satellite in 1994.{{cite web|url=http://www.fakel-russia.com/en/about/|title=ОКБ ФАКЕЛ / About|quote=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|accessdate=26 January 2017|url-status=dead|archiveurl=https://web.archive.org/web/20170206085427/http://www.fakel-russia.com/en/about/|archivedate=6 February 2017}} In 2003, Fakel debuted a second generation of the thruster, called SPT-100B, and in 2011, it presented further upgrades in SPT-100M prototypes.{{cite web|url=http://erps.spacegrant.org/uploads/images/images/iepc_articledownload_1988-2007/2011index/IEPC-2011-041.pdf|title=New Generation of SPT-100|format=PDF|first1=O. A.|last1=Mitrofanova|first2=R. Yu.|last2=Gnizdor|first3=V. M.|last3=Murashko|first4=A. I.|last4=Koryakin|first5=A. N.|last5=Nesterenko|year=2011|id=IEPC-2011-041|accessdate=26 January 2017}} 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.

Specifications

class="wikitable"
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 (%)

|47

|48

|57

|48

Voltage (V)

|300

|300

|300

|600

Discharge current (A)

|4.5

|4.5

|4.5

|4.17

Mass (kg)

|4

|

|

|4.7

colspan="5" style="text-align: left;"|Reference: {{cite web|url=https://ntrs.nasa.gov/search.jsp?R=19930016017|title=Stationary plasma thruster evaluation in Russia|format=PDF|first1=John R.|last1=Brophy|date=15 March 1992|id=19930016017|accessdate=26 January 2017}}{{rp|14}}{{rp|4}}{{cite conference|url=https://iepc2017.org/sites/default/files/speaker-papers/iepc-2017-40_0.pdf|title=High-impulse SPT-100D thruster with discharge power of 1.0...3.0 kW|id=IEPC-2017-40|format=PDF|conference=35th International Electric Propulsion Conference|last1=Gnizdor|last2=Komarov|last3=Mitrofanova|last4=Saevets|last5=Semenenko|accessdate=9 March 2019}}{{rp|6}}

See also

References

{{Reflist}}