In order to investigate the interaction mechanisms between space atomic oxygen (AO) environment and friction material, an AO beam source for space tribology test was developed on the basis of MSTS-1 vacuum tribometer. The radius of beam area is more than Æ50mm, the flux density and energy of the AO beam are 2.6×1015atoms×cm-2×s-1 and 5~10eV, respectively. The typical spacecraft material, i.e. Kapton, is exposed in the simulation facility, and the test results are similar to those of space flight exposure tests. In addition, the performance of the AO source is very stable and can work in high vacuum, the composition of the beam is pure. So the AO source not only satisfies all the special requirements of space tribology test, but also can be used to other space environment simulation test.