Configure Kerwis Chinese Aerospace Pack Engines #2477
Merged
Add this suggestion to a batch that can be applied as a single commit.
This suggestion is invalid because no changes were made to the code.
Suggestions cannot be applied while the pull request is closed.
Suggestions cannot be applied while viewing a subset of changes.
Only one suggestion per line can be applied in a batch.
Add this suggestion to a batch that can be applied as a single commit.
Applying suggestions on deleted lines is not supported.
You must change the existing code in this line in order to create a valid suggestion.
Outdated suggestions cannot be applied.
This suggestion has been applied or marked resolved.
Suggestions cannot be applied from pending reviews.
Suggestions cannot be applied on multi-line comments.
Suggestions cannot be applied while the pull request is queued to merge.
Suggestion cannot be applied right now. Please check back later.
Configure Kerwis Chinese Aerospace Pack Engines.
Due to Chinese rocket development being relatively late, engines have been placed roughly in line with their technological equivalents instead of according to their actual year of development, similar to most European engines.
YF-1: Similar to RD-211, placed in 1957 node
YF-3: Upper stage YF-1, placed in 1958
YF-20: Similar to RD-215/250, placed in 1960 node
YF-22/23/24: Upper stage YF-20, similar to RD-219. Placed in 1960 node
YF-73: Upper stage hydrolox engine. Awful performance and reliability, generally worse than RL10A-1. Placed in 1962 Hydrolox node
YF-75: Upper stage hydrolox engine, similar to RL10A-3-3, placed in 1966 Hydrolox node
YF-77: Gas generator hydrolox sustainer, broadly similar to Vulcain 1/2. Placed in 1996 Hydrolox node
YF-100: Staged combustion booster, directly derived from RD-120K. Placed in 1998 staged combustion node