Abstract
Small rockets can inexpensively aid a number of scientific and operational requirements, such as meteorological sampling, payload component tests, tracking and telemetry systems checkout, and training in the launching and tracking of sounding rockets. The 2.75-in.-diam Folding Fin Aircraft Rocket (FFAR)1has served as a ground-launched radar test rocket for several years at the NASA Wallops Station. The standard inert rocket head has been modified to carry pyrotechnic flares and a smoke-producing chemical to aid radar acquisition using a manual optical sight. In addition, the rocket has been flown with low-drag nose cones, rocket heads weighing 3.8 to 25 lb, and l-in.-diam separable darts. Other organizations have used it for component tests2and as a booster for nonthrusting darts and powered stages3,4.
| Original language | English (US) |
|---|---|
| Pages (from-to) | 938-939 |
| Number of pages | 2 |
| Journal | Journal of Spacecraft and Rockets |
| Volume | 3 |
| Issue number | 6 |
| DOIs |
|
| State | Published - Jun 1966 |
All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Space and Planetary Science
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