Closed zorg2044 closed 5 years ago
Updated
Hmm so this shows Centaur T with both RL10-A3 and RL-10A4-1 (without the nozzle extension so lets call it RL10-A4 in BDB).
Centaur G being an earlier design would have been RL10-A3 of course although if it had been made Im sure it would have gotten the upgrade.
If you wanted to keep it simple I reckon just put down RL10-A4
http://www.b14643.de/Spacerockets_2/United_States_6/Titan_IV/Description/Frame.htm
Just trying to make sense of the various RL10s and to which Centaur they correspond to.
The RL10s
1) RL10 A model with fixed nozzle has 3 B9 subtypes linked to part upgrades
2) RL10-A-4-1N extending nozzle
3) RL10-B-2 bigger extending nozzle
The Centaurs
Centaur D First operational Centaur, 2x RL10-A-3
Centaur D1 Also 2x RL10-A-3
Centaur G/T 2x RL10-A-3 2x RL10-A4 (Centaur T upgrade)
Centaur II (D2) (D2) 2x RL10-A3 (early version, could ignore in the wiki) (D2A) 2x RL10 A4 (D2-A-1-N) later upgraded to 2xRL10-A4-1N with the nozzle extension (D3A) Centaur II was briefly used on early Atlas III. 1x RL10-A4-1N
Common Centaur (aka Centaur III aka D3B for Atlas III and D5for Atlas V) 1 or 2x RL10-A-4-1N (irl the Atlas V used the A-4-2N which had a fixed rather than deploying extension but BDB only has the deployable model)
Suggestions for the wiki
RL10 C is a suffix being used for a whole new series of RL10s being developed that succeed the A4-1 and B-2. It has no bearing on whether its single or dual. In any case these parts arent in BDB.
http://www.b14643.de/Spacerockets_2/United_States_3/Atlas-Centaur/Gallery/Tab.jpg
http://www.b14643.de/Spacerockets/Specials/P&W_RL10_engine/Evolution.gif