Talk:SEPR 84

This article was nominated for deletion on 23 October 2015. The result of the discussion was keep.

This article is within the scope of the Aviation WikiProject. If you would like to participate, please visit the project page, where you can join the project and see lists of open tasks and task forces. To use this banner, please see the full instructions.AviationWikipedia:WikiProject AviationTemplate:WikiProject Aviationaviation

This article has been checked against the following criteria for B-class status:
Referencing and citation: criterion not met Coverage and accuracy: criterion not met Structure: criterion met Grammar and style: criterion not met Supporting materials: criterion met

This article is supported by the aircraft engine task force.

Quoted Mass Flowrate is Incorrect

Latest comment: 3 years ago1 comment1 person in discussion

The "propellant consumption" value given (0.00435 lb/s) is infeasibly low and would correspond to an efficiency roughly 1000 times higher than any known propellant combination. This paper gives a reasonable value of 7.15 kg/s, if it counts as a trustworthy source https://www.ibb.ch/spl_old/news/SEPR/AIAA-90-1835.pdf 104.244.222.100 (talk) 04:46, 5 January 2023 (UTC)Reply

This page was redesigned at the edge.

A page that knows where it met you.

Talk:SEPR 84

Quoted Mass Flowrate is Incorrect