Jump to content

SABRE (rocket engine): Revision history


For any version listed below, click on its date to view it. For more help, see Help:Page history and Help:Edit summary. (cur) = difference from current version, (prev) = difference from preceding version, m = minor edit, → = section edit, ← = automatic edit summary

(newest | oldest) View (newer 50 | ) (20 | 50 | 100 | 250 | 500)

27 April 2024

2 March 2024

18 August 2023

17 August 2023

14 August 2023

27 January 2023

6 January 2023

24 December 2022

21 November 2022

6 September 2022

1 September 2022

31 August 2022

25 August 2022

24 August 2022

22 June 2022

20 June 2022

18 June 2022

11 June 2022

24 April 2022

  • curprev 11:0111:01, 24 April 2022Richardthefifth talk contribs 42,965 bytes +553 Article correctly referred to completion of test facility by 2020, but by now (2022) this information is clearly out of date. Updated to state that the site has instead been taken over by Nammo. undo

30 January 2022

2 January 2022

16 October 2021

9 April 2021

27 March 2021

26 February 2021

8 January 2021

  • curprev 03:4403:44, 8 January 2021Jlefevre76 talk contribs 42,278 bytes +213 My CAD job is making me less creative, I forgot about counterflow heat exchangers, and couldn't figure out how both the helium and air exited the engine at 150 C (they don't, because it's a counterflow heat exchanger). Just in case some of the rest of the engineers working in other fields forget about counterflow heat exchangers, I added a note to clarify how it can adequately transfer the heat. undo Tags: Visual edit Mobile edit Mobile web edit

11 December 2020

10 December 2020

9 December 2020

4 December 2020

(newest | oldest) View (newer 50 | ) (20 | 50 | 100 | 250 | 500)