HR-715 - First published in NASA-STD-8719.29. First used in Software Engineering Handbook Version D.
| SWEHB Rev | HR Rev | Requirement Statement |
|---|---|---|
| D | Baseline | 4.7.1.5 If a range safety destruct system is incorporated into the design, the space system shall automatically initiate the Earth ascent abort sequence when range safety destruct commands are received onboard, with an adequate time delay prior to destruction of the launch vehicle to allow a successful abort. |
