The parameter’s optimization of the meteorological rocket’s correcting engine to reduce the zone of the used blocks’ falling
On the example of the meteorological rocket MMR-06, the optimum parameters of the trajectory correction engine to reduce the zone of the used blocks’ falling was selected. It is shown that the optimum mass and optimal maneuvering time are achieved for engines with the medium-thrust. Low-thrust engin...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
EDP Sciences
2017-01-01
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| Series: | MATEC Web of Conferences |
| Online Access: | https://doi.org/10.1051/matecconf/201712906007 |