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I recently took a photo of the M-1 and have added it to the article. It is interesting to note that the SVG 'scale' drawing is much larger than the actual engine in the photo. I'm assuming that the nozzle extension must have been very large in the diagram depicted, but absent in the museum display.
As you can see from the thumbnails added on the right, these two depictions are quite different.
I will leave the page as is for comment. - Kyle (talk) 06:35, 28 April 2014 (UTC)
According to F-1, the F-1A rocket produced over 2 million lb-f thrust, more than the M-1. Also this article would make it appear that since no hydrogen pumps were tested, no M-1 was ever completed, whereas the F-1A would appear to have been completed but never flown. 74.134.236.69 06:41, 29 October 2006 (UTC)
This is the
talk page for discussing improvements to the
Aerojet M-1 article. This is not a forum for general discussion of the article's subject. |
Article policies
|
Find sources: Google ( books · news · scholar · free images · WP refs) · FENS · JSTOR · TWL |
This article is written in American English, which has its own spelling conventions (color, defense, traveled) and some terms that are used in it may be different or absent from other varieties of English. According to the relevant style guide, this should not be changed without broad consensus. |
This article is rated Start-class on Wikipedia's
content assessment scale. It is of interest to the following WikiProjects: | |||||||||||||||||||||||||||||||
|
I recently took a photo of the M-1 and have added it to the article. It is interesting to note that the SVG 'scale' drawing is much larger than the actual engine in the photo. I'm assuming that the nozzle extension must have been very large in the diagram depicted, but absent in the museum display.
As you can see from the thumbnails added on the right, these two depictions are quite different.
I will leave the page as is for comment. - Kyle (talk) 06:35, 28 April 2014 (UTC)
According to F-1, the F-1A rocket produced over 2 million lb-f thrust, more than the M-1. Also this article would make it appear that since no hydrogen pumps were tested, no M-1 was ever completed, whereas the F-1A would appear to have been completed but never flown. 74.134.236.69 06:41, 29 October 2006 (UTC)