L. L. Scalzott

Thrust vector control requirements for launch vehicles using a 260-inch solid rocket first stage

C. J. Daniele, J. Borsody, L. L. Scalzott, 1969 .

Load relief autopilot analysis to minimize launch vehicle peak thrust vector deflection requirements

F. Teren, L. L. Scalzott, 1968 .

Practical stability criterion and its application to digital simulation

L. L. Scalzott, C. F. Lorenzo, 1967 .