Study of shuttle imaging microwave system antenna. Volume 1: Conceptual design [PDF]
A detailed preliminary design and complete performance evaluation are presented of an 11-channel large aperture scanning radiometer antenna for the shuttle imaging microwave system (SIMS) program.
Barton, C. R. +3 more
core +1 more source
A perspective on competitive freeride skiing and snowboarding. [PDF]
Mulder E, Holmberg HC, Supej M.
europepmc +1 more source
Surface-energy ratchet motor with geometrical symmetry driven by biased random walk. [PDF]
Hatatani M, Yamamoto D, Shioi A.
europepmc +1 more source
Towards a Steerable Neurosurgical Robot for Debulking of Brain Mass Lesions. [PDF]
Saini S +4 more
europepmc +1 more source
Lessons Learned in Fabrication of a High-Specific-Torque Concentric Magnetic Gear [PDF]
Magnetic gearing is being investigated at NASA as a replacement to conventional mechanical gearing in aerospace applications. Some key benefits of magnetic gears over mechanical gearing are torque transmission without mechanical contact, decreased ...
Cameron, Zachary A. +2 more
core +1 more source
Neuromuscular Responses to 5 K Time Trial Load Carried by Spanish Army Marines. [PDF]
Cáceres-Diego B +2 more
europepmc +1 more source
Application of active control landing gear technology to the A-10 aircraft [PDF]
Two concepts which reduce the A-10 aircraft's wing/gear interface forces as a result of applying active control technology to the main landing gear are described.
Edson, R., Ross, I.
core +1 more source
Effectiveness analysis of a novel rectangular tunnel boring machine with planetary transmission for box jacking. [PDF]
Ma P, Zhao Y, Shimada H, Zhou H.
europepmc +1 more source
MR conditional prostate intervention systems and actuations review. [PDF]
Liang H, Tse ZTH.
europepmc +1 more source
Aerodynamic design of a free power turbine for a 75 KW gas turbine automotive engine [PDF]
A single stage axial-flow turbine having a tip diameter of 15.41 centimeters was designed. The design specifications are given and the aerodynamic design procedure is described. The design includes the transition duct and the turbine exit diffuser.
Katsanis, T. +2 more
core +1 more source

