The YF-1 was a Chineseliquidrocket engine burning N2O4 and UDMH in a gas generator cycle. It is a basic engine which when mounted in a four engine module forms the YF-2. It was used as the basis for developing a high altitude version known as the YF-3.[2][9]
Some authors state that it was a direct copy of С.2.1100/С.2.1150 La-350 booster engine developed by IsayevOKB-2 (NII-88).[10] What is known is that the engine development had great trouble with combustion instabilities and it took a long time to have a reliable combustion.
Versions
The basic engine has been used since the DF-3 rocket and has been the main propulsion of the Long March 1 orbital launch vehicles.[2]
YF-1: Core engine. Flown originally on the DF-3. Used UDMH/AK27S as propellant. Allegedly a copy of OKB-2's С.2.1150.[3][10]
YF-3A: Improved upper stage version. Used on the Long March 1.[2]
Modules
While the basic engine was used multiple times, it was only used as a single engine for booster application. It is usually bundled into modules of multiple engines.
The relevant modules for first stage application are:
YF-2: A module comprising four YF-1. Flown originally on the DF-3.[3]