Talk:SpaceX reusable launch system development program: Difference between revisions

Revision as of 04:58, 23 May 2018

Revision as of 14:21, 8 November 2018

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The "Second-stage reuse" section of the article currently states an, "integrated second-stage-with-spaceship design [...] has not been commonly used in previous launch vehicles." But see [[RM-81 Agena]]. The final launch was in 1987; 365 were flown. Does that flight history somehow fail to qualify Agena as having been "commonly used?" ([[User:Sdsds|sdsds]] - ''[[User talk:Sdsds|talk]]'') 06:15, 22 May 2018 (UTC)

:Just saw this question [[User:Sdsds|sdsds]]. Is a good one. I had time only to skim that Wikipedia article prose, but not go after the sources. Do you think there is a good source anywhere that does a solid job explicating just how the Agena might be thought to have been an "integrated second-stage-with-spaceship design"? Otherwise, it seems a bit like Agena, and maybe even a few of the Chinese second stages being used today, are more "integrated second-stage-with-attached satellite" designs. But even that might be worth mentioning to improve this article if we could find sources that are descriptive of some sort of integrated-second-stage designs in contrast to the BFR design integrated reusable spaceship designs. Cheers. [[User:N2e|N2e]] ([[User talk:N2e|talk]]) 14:20, 8 November 2018 (UTC)