The Wayback Machine - https://web.archive.org/web/20161228032847/http://astronautix.com/t/tal-38.html
TAL-38

Encyclopedia Astronautica
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
TAL-38
Part of TAL Family
TAL-38
TAL-38
TAL-38 HAL effect thruster
Credit: TsNIIMASH
TsNIIMash electric/xenon rocket engine. Development. Hall effect thruster with anode layer. Export version of D-38, developed under NASA contract for satellite station-keeping and attitude control. Taken to engineering model stage.
See More

AKA: D-38. Status: Development. Thrust: 0.0080 N (0.0017 lbf). Specific impulse: 2,500 s.

Thrust 2.5 to 8 mN, power requirement 0.4 to 1.0 kW, specific impulse 1300-2500 seconds, efficiency 45%.

Electrical Input Power: 1.00 kW.

Country: Russia. Propellants: Electric/Xenon. Agency: TsNIIMash.

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
� 1997-2016 Mark Wade - Contact
� / Conditions for Use