@techreport{oai:jaxa.repo.nii.ac.jp:00006261,
 author = {矢部, 高弘 and 川崎, 春夫 and Yabe, Takahiro and Kawasaki, Haruo},
 month = {Jan},
 note = {This report describes the development of a small-sized mechanical pump. The pump can be used in thermal control systems, such as Mechanical Pumped Loops (MPL) of spacecraft. This pump has following three features. (1) Ammonia used as working fluid. (2) Small sized design for spacecraft. (3) Axial type motor used for driving gear. The trochoid gear miniaturized the pump with the external diameter of 48 mm, the thickness of 19 mm and weight of 150 g. As a result of the performance test, 0.5 L/min flow rate, 45 kPa of total pressure and 2 MPa withstand pressure were achieved., 資料番号: AA0049054005, レポート番号: JAXA-SP-05-008},
 title = {宇宙用アンモニア小型流体駆動源の初期開発検討},
 year = {2006}
}