Display
location: History Center
Type: Vernier engine designated LR
101-NA-7 or MA-3 Vernier
Contractor: Rocketdyne Corporation
Related exhibits:
Used
on Atlas rockets to provide roll control during flight and final
velocity and attitude corrections after sustainer cutoff. This model
was used on Atlas E and Atlas F series (SM-65). Ignited about 3.5
seconds after booster engines and sustainer were started. Controlled
roll, pitch and yaw trim during spacecraft coasting flight. Made
precise attitude adjustments, especially to solid fuel rockets,
which are difficult to throttle and steer. Helped attain separation
between stages and to "settle" liquid propellants which prevented
sloshing and frothing. Capable of operating at temperatures between
-30 degrees and +130 degrees Fahrenheit.
Position of the two vernier engines on an Atlas is shown at left.