A coupled computer code for the transient thermal response and ablation of non-charring heat shields and nose tips
Coupled computer code for transient thermal response and ablation of noncharring heat shields and nose tips
Anderson, L. W.↗
Engineering topics
Dahm, T. J.
Publications and source records attributed to Dahm, T. J..
Studies of ablative material performance for solid rocket nozzle applications
Ablative materials performance for solid rocket nozzle applications
Dahm, T. J.↗
Studies of nozzle ablative material performance for large solid boosters Final report
Carbon phenolic, graphite phenolic, and silica phenolic nozzle ablative materials performance for large solid propellant rocket boosters
NOZZLE EFFICIENCY↗