The Wayback Machine - https://web.archive.org/web/20161228054105/http://astronautix.com/t/tal-100.html
TAL-100

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-100
Part of TAL Family
TAL-100
TAL-100
TAL-200 HAL effect thruster
Credit: TsNIIMASH
TsNIIMash electric/xenon rocket engine. Development. Hall effect thruster with anode layer. Export version of D-100-I thruster developed under NASA/BMDO contract. Taken to engineering model stage.

AKA: D-100. Status: Development. Thrust: 0.0340 N (0.0070 lbf). Specific impulse: 1,450 s.

Used for satellite orbital altitude maintenance and raising. Thrust 8 to 34 mN, power requirement 1.3 to 7.5 kW, specific impulse 1450-2800 seconds, efficiency 60%.

Electrical Input Power: 7.50 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