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Numerous other items of interest are mentioned on the Guide, with launch vehicle specific elements such as a large common bulkhead being employed on the second stage and common tooling on the second stage and that is also aluminum orthogrid material in its construction. The rocket will use autogenous pressurization for both stages.
The large 7 meter fairing has the ability to launch very large payloads such as space telescopes, but also dual payloads – not unlike Ariane 5 regularly conducts.
The Guide refines some performance numbers, with 1060 kN (240,000 lb) total thrust cited for the second stage, which is slightly down from the 125,000 lb per BE-3U – the second stage engine-performance previously stated by Blue Origin’s online resources.
The article at the link also provides some updates on the status of the construction of the rocket’s launchpad, landing barge, and manufacturing facility.