Quote from: patchfree on 08/27/2009 05:47 pm "whereas Russian projects are delayed, descoped, but rarely vanish."Hum... I am a fan of soviet and russian space but I would remind that they cancelled 2 enormous projects at the final phase: LV lunar N1 and Energia-Buran!! Now fortunately they are more pragmatic (money!)PatchPerhaps I was not being sufficiently precise in my statement. The lunar program and Energia/Buran did not exactly vanish in these sense of X-33, NASP, etc. Both programs produced both flight tests and resulting technologies used today. In fact, Energia/Buran was canceled in the sense that Apollo was canceled, as the Russian program met its program goals and then was killed.The Zenit rocket is a result of Energia/Buran. It still flies today.
"whereas Russian projects are delayed, descoped, but rarely vanish."Hum... I am a fan of soviet and russian space but I would remind that they cancelled 2 enormous projects at the final phase: LV lunar N1 and Energia-Buran!! Now fortunately they are more pragmatic (money!)Patch
Quote from: fregate on 09/04/2009 10:41 amWhat is that thing on the right? The configuration looks all wrong for it to be an LV. Is it some kind of deep space transfer vehicle?
Launch vehicle for next-generation spacecraft.The MAKS 2009 pavilion of the Roscosmos Federal Space Agency features a mock-up of the Rus-M two-stage heavylift launch vehicle under development by the Samara-based TsSKB-Progress design bureau.The Rus-M is intended for carrying new-generation manned craft and resupply vehicles to the orbit from Russia’s new Vostochny cosmodrome. TsSKB-Progress is co-developing the preliminary design with the Energia Rocket and Space Corporation and the Makeev design bureau. Thelaunch vehicle is a modular design, with the first stage using three URB-1 blocks with Energomash RD-180 oxygen/kerosene engines. The second stage’s four RD-0146 engines run on a liquid cryogenic fuel of oxygen and hydrogen.With an all-up weight of 673 tons, the Rus-M can insert a 23.8-ton payload into low earth orbit. If an additional upper stage is used, the rocket can deliver a satellite weighing 4 tons into geostationary orbit.Development testing is set to begin in 2015. From 2018 the rocket should start launching new-generation manned spacecraft.
Let me get one thing straight: The baseline for this LV is the tri-core version shown in that model? There is no EELV-style single-core version?
Have they really done any work on a NEP tug, or is it just pie-in-the-sky PR?Because it looks VERY similar to NASA's JIMO (Jupiter Icy Moon Orbiter) spacecraft project that was cancelled in 2005: http://en.wikipedia.org/wiki/Jupiter_Icy_Moons_Orbiter