Dave Limp (@davill)

Launch table is out. The two-million-pound launch table is heading to the Integration Facility for inspection and adjustments to support our future ConOps. Once reinstalled at the pad, it'll be outfitted with the first stage aft umbilicals and tied into the water system, which delivers water injection just below the engine nozzles.

We're not rebuilding the same pad for New Glenn. We're moving to a horizontal/vertical hybrid configuration to get us flying again this year at 36A.  We were already working on something similar for 9x4 at 36B. Let me explain what that means. We mate the stages horizontally in the Integration Facility (IF). Then we bring the integrated vehicle out to the pad, use a crane to perform the vertical breakover, and mate the payload once New Glenn is vertical. This new ConOps has the added benefit of increasing our flight cadence as well.

I've come to appreciate boring hotfires. Our BE-7 team recently completed a 2,500 second hotfire test at 10klbf on a development engine, setting the record for the longest-duration turbo pump-fed liquid rocket engine hotfire. This built on some of the most rigorous testing in the history of propulsion, with the previous record set by the RS-25 engine that powered the Space Shuttle. They recorded two 2,017 second tests in 1988. It's not lost on us that we're following a path those engineers blazed, and we're grateful for it. Grab the popcorn and enjoy watching 41 minutes of hotfire goodness.

Some LC-36 updates. Now that we’ve had access to the pad and integration facility we can share a bit of good news. The propellant farm, oxygen, liquid hydrogen and LNG tanks are all in good shape. This is good luck because these are very long lead items. The water tower is also good. The big support tower is damaged, but it can be repaired in place rather than torn down and replaced. The booster “Never Tell Me The Odds” and the three GS-2s that were onsite in the integration facility also look good. I’ve seen some speculation that we might move directly to the 9x4 configuration, but we won’t do that. Rate manufacturing of 7x2 is going well, and we’re going to continue that at pace as planned and store the stages for use. In addition, we had already been working for some time on eliminating our transporter-erector in favor of an alternative vertical conop, and we’ll now go directly to that; so we don’t need a new transporter-erector. We will fly again before the end of this year. Gradatim Ferociter.