Abstract
The article discusses the problem of employing balance forces produced by a device located in a missile, when the missile is affected by inertial forces due to a change in its direction, to lower the effect of the inertial forces to the maximum extent.
| Original language | English |
|---|---|
| Pages (from-to) | 446-448 |
| Number of pages | 3 |
| Journal | Journal of Spacecraft and Rockets |
| Volume | 14 |
| Issue number | 7 |
| DOIs | |
| State | Published - 1 Jan 1977 |
ASJC Scopus subject areas
- Aerospace Engineering
- Space and Planetary Science
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