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| PLASMA-JET ENGINE WITH CLOSED-CIRCUIT ELECTRON DRIFT |
| FIELD: space engineering; stationary plasma jet engines and anode-layer engines of electric rocket engine units.
EFFECT: enhanced reliability and service life of engine. 2 cl, 2 dwg |
| Publishing date: October 8, 2002 |
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| A METHOD TO INJECTION A USEFUL LOAD TO SPACE ORBIT |
| A method applied today to inject a useful load to a space orbit includes flight preparation and take-off of a multimode accelerating aircraft, carrying a booster rocket, from an airdrome; a flight to the booster rocket launching area with aircraft refilling in the air or without refilling; acceleration and climb upon approaching the booster rocket launching area; accelerating aircraft switch-over to a command-measuring mode; launching object monitoring till the time it successfully reaches a targeted orbit (with or without refilling); and a return to a landing airdrome.
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| Publishing date: January 10, 2001 |
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| METHOD OF DETECTING THE LEAKAGE OF THE SPACE VEHICLE BODY WHILE ON THE ORBIT |
| The method consists in creating
the medium pressure inside the space vehicle body, and the leakage is judged
from the behavior of the fiber-containing sensitive element. |
| Publishing date: July 21, 2000 |
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