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TAL
Transatlantic Abort Landing (Shuttle abort plan)
Subtopics
| Hall Electric Thruster TsNIIMash / Rocketdyne electric/xenon rocket engine. Development. Satellite orbit raising and station-keeping applications. Electric, pressure-fed. Variable 80 mN - 3.0 N thrust, specific impulse 1600 to 3500 seconds. |
| D-20 TsNIIMash electric/xenon rocket engine. Development. Hall effect thruster with anode layer, designed for satellite station-keeping and attitude control. Taken to engineering model stage. |
| D50 Yuzhnoye electric/xenon rocket engine. Development. Hall engine electric jet propulsion system intended for use by spacecraft for inter-orbital transfer, orbit correction, and stabilization. |
| D-100-II TsNIIMash electric/xenon rocket engine. Development. Hall effect thruster with anode layer, designed for satellite orbital raising. Taken to engineering model stage. |
| TAL-100 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. |
| TM-50 TsNIIMash electric/xenon rocket engine. Development. Hall effect thruster with anode layer, designed for satellite orbital raising. Taken to engineering model stage. |
| TAL-38 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. |
| TAL-WSF TsNIIMash electric/xenon rocket engine. Hall effect thruster with anode layer. Export version of D-55 thruster developed under NASA/BMDO contract for flight test under RHETT-II program. Used for WSF satellite orbital altitude maintenance. |
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