ULA Next Generation Launch System


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SpaceFlightInsider has an interview with ULA CEO Tori Bruno, the subject being their Next Generation Launch System, the replacement for Atlas V and Delta IV which is planned to fly in 2019.

To cut costs they'll be cutting back to 2 launch facilities, 1 per coast, and of the BE-4 doesn't work out the backup is apparently the yet to be built Aerojet-Rocketdyne AR-1 ($25m+ a pair).

Downside: if a launch goes kaboom they risk months of delays like Orbital Sciences after the Antares incident

http://www.spaceflightinsider.com/organizations/ula/insider-interview-united-launch-alliances-tory-bruno-next-generation-launch-system/#comment-554615

Not all in the article,

5 meter core (Delta IV diameter)

S1: 2x Blue Origin BE-4

Propellant: LNG/LOX

S2 (initial LH2): Delta Cryogenic Second Stage

S2 (evolved LH2): Blue Origin BE-3U, XCOR, or ACES**

SRB's: Aerojet-Rocketdyne

Existing payload fairings

Recycling as much h/w as possible

Possible 3-core Heavy variant to replace Delta IV Heavy

** http://en.m.wikipedia.org/wiki/Advanced_Common_Evolved_Stage

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Bruno is going to discuss reusability at an upcoming conference.

IMO he'll either try to debunk it and SpaceX's efforts on economic grounds, or announce they'll support Blue Origin's R&D. The middle road of ignoring the Kodiak bear in the room obviously isn't working.

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Debunking it would also kind of be a slapping their partners over at Blue Origin in the face wouldn't it? I mean I know they are currently only in bed concerning that new BE-4 engine, but still...

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I think they'll support BO.

It's hard to get news out of BO because they're so secretive, but they have people from the DC-X program. They've also done landing avionics work using both subscale booster-like testbeds (about 1/3 the size of Dev-1), and before that landers powered by small vertical turbojets.

Blue Origin RLV testbed

settled_500_375.jpg

blueorigin-pm2.jpg

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