FIELD: test equipment.
SUBSTANCE: invention relates to the field of experimental aerodynamics and can be used for tests of space flight vehicles and rockets. The prechamber differs by that is contains the screen designed as thin-walled perforated shell. The screen is located with a gap near the prechamber walls.
EFFECT: decrease of dust content of the working flow.
1 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
PRECHAMBER OF PISTON WIND TUNNEL | 1969 |
|
SU1840954A1 |
PRECHAMBER OF ADIABATIC COMPRESSION AERODYNAMIC TUNNEL | 1965 |
|
SU1840311A1 |
0 |
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HIGH-TEMPERATURE PRECHAMBER OF DUAL-CHAMBER ADIABATIC COMPRESSION UNIT | 1971 |
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METHOD OF START OF AIRCRAFT WITH ACCELERATION AT INITIAL FLIGHT PATH | 1984 |
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SU1840857A1 |
Authors
Dates
2014-10-27—Published
1967-12-21—Filed