1-24 of 26 Books
Performance of a low-power subsonic-arc-attachment arcjet thruster
Performance of a low-power subsonic-arc-attachment arcjet thruster
By John M. Sankovic
Nuclear thermal propulsion
Nuclear thermal propulsion
By Nuclear Thermal Propulsion Workshop (1990 Cleveland, Ohio)
7.5K lbf thrust engine preliminary design for orbit transfer vehicle
7.5K lbf thrust engine preliminary design for orbit transfer vehicle
By Warren R. Hayden
Advanced Earth-to-orbit propulsion technology information, dissemination, and research
Advanced Earth-to-orbit propulsion technology information, dissemination, and research
By S. T. Wu
Rocket-based combined cycle engine technology development
Rocket-based combined cycle engine technology development
By J. R. DeBonis
Solid-propellant rocket motor internal ballistics performance variatio analysis (phase five)
Solid-propellant rocket motor internal ballistics performance variatio analysis (phase five)
By Richard H. Sforzini
Arcjet thruster research and technology
Arcjet thruster research and technology
By Rocket Research Company.
Robust rocket engine concept
Robust rocket engine concept
By Carl F. Lorenzo
Design Methods in Solid Rocket Motors
Design Methods in Solid Rocket Motors
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
SRB thermal curtain design support
SRB thermal curtain design support
By Wayne E. Lundblad
Advanced small rocket chambers option II
Advanced small rocket chambers option II
By Donald M. Jassowski
Propellant injection systems and processes
Propellant injection systems and processes
By Jackson I. Ito
Micro electric propulsion feasibility
Micro electric propulsion feasibility
By Graeme Aston
"Fast Track" NTR systems assessment for NASA's first lunar outpost scenario
"Fast Track" NTR systems assessment for NASA's first lunar outpost scenario
By Stanley K. Borowski
Developments in REDES
Developments in REDES
By Kenneth O. Davidian
Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle
Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle
By R. W. Marable
Program test objectives milestone 3
Program test objectives milestone 3
By T. L. Gaynor
Recycle requirements for NASA's 30cm xenon ion thruster
Recycle requirements for NASA's 30cm xenon ion thruster
By Luis R. Piñero
The effect of cooling passage aspect ratio on curvature heat transfer enhancement
The effect of cooling passage aspect ratio on curvature heat transfer enhancement
By Michael L. Meyer
Electrically heated tube investigation of cooling channel geometry effects
Electrically heated tube investigation of cooling channel geometry effects
By Michael L. Meyer
Predicted performance of an integrated modular engine system
Predicted performance of an integrated modular engine system
By Michael P. Binder
A transient model of the RL10A-3-3A rocket engine
A transient model of the RL10A-3-3A rocket engine
By Michael P. Binder
2004 NASA Seal/Secondary Air System workshop
2004 NASA Seal/Secondary Air System workshop
By NASA Seal/Secondary Air System Workshop (2004 NASA Glenn Research Center)