Table 8.
Focal length variation due to launch environment dynamics.
| f [mm] | [mm] | |
|---|---|---|
| Before tests | 25.287 | 0 |
| After vibration | 23.968 | −1.3190 |
| After shock | 24.283 | +0.3150 |
Official websites use .gov
A
.gov website belongs to an official
government organization in the United States.
Secure .gov websites use HTTPS
A lock (
) or https:// means you've safely
connected to the .gov website. Share sensitive
information only on official, secure websites.