14 C.F.R. § 420.21
(c) For a launch site supporting any reusable launch vehicle, an applicant shall determine the debris dispersion radius that represents the maximum distance from a launch point that debris travels given a worst-case launch vehicle failure in the launch area. An applicant must clearly and convincingly demonstrate the validity of its proposed debris dispersion radius.
| Orbital expendable launch vehicle class | Type of suborbital launch vehicle | ||||
|---|---|---|---|---|---|
| Small | Medium | Medium large | Large | Guided | Unguided |
| 7300 | 9300 | 10600 | 13000 | 8000 | 1600 |