FIELD: engine sets. SUBSTANCE: solar heat rocket engine has radiation detector in the form of two concentric tubes 2, 3, concentrator 1 with longitudinal center line, whose shape provides for focusing of sun rays on entire length of external tube 2 of detector. Working medium heated in detector goes to nozzle 7. EFFECT: design. 3 dwg
Title | Year | Author | Number |
---|---|---|---|
COMBINED ELECTRIC JET-PROPULSION ENGINE UNIT FOR SPACECRAFT, METHOD OF CREATING CONTROLLING MOMENTS AND THREE-CHANNEL ELECTRIC JET-PROPULSION ENGINE | 1992 |
|
RU2040445C1 |
METHOD OF UNLOADING POWER GYROSCOPE SYSTEM OF SPACE VEHICLES | 1991 |
|
RU2028256C1 |
CONCENTRATING DEVICE | 1991 |
|
RU2027120C1 |
APPARATUS FOR CLEANING SPACE OF FOREIGN MATTER | 1992 |
|
RU2040449C1 |
ACCUMULATING HEAT RECEIVER OF POWER PLANT | 1991 |
|
RU2027122C1 |
METHOD OF FORMING UNLOADING MOMENT FOR POWDERED GYROSCOPE SYSTEM OF SPACE VEHICLE WITH SOLAR-CELL BATTERIES | 1992 |
|
RU2030338C1 |
METHOD OF MAKING ICE IN ICE PACK ON BOARD SPACE VEHICLE AND DEVICE FOR ITS REALIZATION | 1992 |
|
RU2040444C1 |
SPACECRAFT ATTITUDE CONTROL SYSTEM | 1992 |
|
RU2006431C1 |
PRESSURE DROP GAUGE | 1992 |
|
RU2029934C1 |
STEERING GEAR | 1991 |
|
RU2014246C1 |
Authors
Dates
1995-02-09—Published
1990-05-07—Filed