A solid chemical rocket propulsion system includes a solid fuel and a solid oxidizer that is physically separated from the solid fuel and is not mixed with solid fuel while the rocket is initially at rest.
申请公布号
US2014109551(A1)
申请公布日期
2014.04.24
申请号
US201313828371
申请日期
2013.03.14
申请人
LOS ALAMOS NATIONAL SECURITY, LLC;RISHA GRANT A.;LOS ALAMOS NATIONAL SECURITY, LLC
