Rocket engine design

Saturn V: the complete manufacturing and test records : plus supplemental material

Alan Lawrie & Robert Godwin.

The effect of cooling passage aspect ratio on curvature heat transfer enhancement

Michael L. Meyer.

Arcjet thruster research and technology: phase II final report, NAS 3-24631

prepared by Rocket Research Company.

SRB thermal curtain design support: October 1990 interim report to U.S. Polymeric, B.P. Chemicals

prepared by Wayne E. Lundblad.

Advanced small rocket chambers option II: fundamental processes and material evaluation : final report

Donald M. Jassowski.

Thermal stratification potential in rocket engine coolant channels

Kenneth J. Kacynski.

Performance of a low-power subsonic-arc-attachment arcjet thruster

John M. Sankovic and Darren H. Berns.

Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle

R. W. Marable

A transient model of the RL10A-3-3A rocket engine

Michael P. Binder.

7.5K lbf thrust engine preliminary design for orbit transfer vehicle: task D.5 final report

Warren R. Hayden, Ralph Sabiers, and Judy Schneider.