Samanta Roy, 1995 - Google Patents
Numerical simulation of ion thruster plume backflow for spacecraft contamination assessmentSamanta Roy, 1995
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- 3595706465118877586
- Author
- Samanta Roy R
- Publication year
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In order to accurately assess the backflow contamination potential of electric propulsion thrusters for spacecraft-thruster integration purposes, models of the plumes and backflow are necessary. The effluents of ion thrusters, Hall or Stationary Plasma Thrusters (SPT) …
- 150000002500 ions 0 title description 477
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/52—Protection, safety or emergency devices; Survival aids
- B64G1/58—Thermal protection, e.g. heat shields
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