Vernier thruster (English Wikipedia)

Analysis of information sources in references of the Wikipedia article "Vernier thruster" in English language version.

refsWebsite

Global rank English rank

75^th place

83^rd place

1^st place

low place

2,428^th place

1,659^th place

heroicrelics.org

"Rocket Control: Examples of Controls". NASA's Glenn Research Center. Archived from the original on March 7, 2011. Retrieved December 30, 2011.

"Reaction Control Systems". NASA Kennedy Spaceflight Center. Retrieved 2011-10-03. The flight crew can select primary or vernier RCS thrusters for attitude control in orbit. Normally, the vernier thrusters are selected for on-orbit attitude hold. ... The forward RCS had 14 primaries and two vernier engines. The aft RCS had 12 primary and two vernier engines in each pod. The primary RCS engines provided 870 pounds of vacuum thrust each, and the verniers provided 24 pounds of vacuum thrust each. The oxidizer-to-fuel ratio for each engine is 1.6-to-1. The nominal chamber pressure of the primary thrusters was 152 psia. For each vernier, it was 110 psi.

Bergin, Chris (19 February 2010). "STS-130 prepares for undocking – MMOD impact on hatch cleared". NASAspaceflight.com. Retrieved 20 February 2010.

"Rocket Control: Examples of Controls". NASA's Glenn Research Center. Archived from the original on March 7, 2011. Retrieved December 30, 2011.