Jump to content

Electromagnetic Aircraft Launch System: 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)

4 May 2025

16 April 2025

4 April 2025

18 March 2025

17 March 2025

13 February 2025

  • curprev 20:1220:12, 13 February 2025 2601:681:8a00:c130:20c2:f9e8:27e2:eafa talk 31,239 bytes −8 Reliability: The source says EMALS has approximately 240 Mean Cycles Between Critical Failure. The author incorrectly explained this as an average time between failure (usually called mean time between failure or MTBF) and then expressed said MTBF incorrectly as a rate instead of a time (usually hours). The edit fixes the MTBF issue and expresses the failure rate as a failure rate. 1 failure/240 cycles is the correct failure rate as it is the inverse of 240 mean cycles/ failure. undo Tags: Mobile edit Mobile web edit

17 November 2024

6 November 2024

9 October 2024

8 October 2024

15 September 2024

14 September 2024

26 August 2024

2 March 2024

17 February 2024

2 December 2023

30 November 2023

15 October 2023

18 July 2023

30 June 2023

27 April 2023

6 February 2023

5 February 2023

25 December 2022

2 November 2022

11 October 2022

7 October 2022

5 October 2022

27 September 2022

20 September 2022

19 September 2022

23 August 2022

17 August 2022

20 July 2022

17 July 2022

24 June 2022

23 June 2022

19 June 2022

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