A. O. Pearson

Wind-Tunnel Investigation at Mach Numbers from 0.60 to 1.20 of the Static Aerodynamic Characteristics of a Model of a Possible Nonlifting Reentry Capsule in Combination with a Rocket Booster

A. O. Pearson, 1960 .

Preliminary results from an operational 90-day manned test of a regenerative life support system

A. O. Pearson, D. C. Grana, 1971 .

Contributions of a developmental integrated life support system to aerospace technology.

G. L. Drake, J. N. Pecoraro, A. O. Pearson, 1967 .

SURFACE PRESSURE DISTRIBUTIONS ON 0.0628-SCALE MODELS OF PROPOSED PROJECT FIRE SPACE VEHICLES AT MACH NUMBERS FROM 0.25 TO 4.63

A. O. Pearson, 1963 .

Summary of a 90-Day Manned Test of a Regenerative Life Support System

A. O. Pearson, J. K. Jackson, 1973 .

WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.40 TO 1.20 OF THE STATIC AERODYNAMIC AND CONTROL CHARACTERISTICS OF A MODEL OF A NONLIFTING REENTRY CAPSULE IN COMBINATION WITH A ROCKET BOOSTER

A. O. Pearson, 1960 .