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India Ferrah is the stage name of Shane Richardson, an American drag queen and costume designer best known for competing on the third season of RuPaul's Drag Race. Richardson was raised in Roanoke, Virginia , and came out as gay and started performing in drag as India Ferrah during his teens.
Shane Richardson is the CEO of the Australian National Rugby League team, the Wests Tigers. Richardson started with the Cronulla-Sutherland Sharks [1] in 1993 and stayed for five years before joing Hull F.C. in the English Super League. Richardson returned in 2002, joining the Penrith Panthers, and then the South Sydney Rabbitohs in 2004.
Shane Richardson may refer to: Shane Richardson (rugby league), Australian rugby league administrator; Shane Richardson (American football), American football coach ...
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For more complicated maneuvers which may involve a combination of change in inclination and orbital radius, the delta-v is the vector difference between the velocity vectors of the initial orbit and the desired orbit at the transfer point. These types of combined maneuvers are commonplace, as it is more efficient to perform multiple orbital ...
Shane Richardson is an American college football coach and former player. He is the head football coach for Northern Michigan University , a position he has held since 2023. He served as the head football coach at the University of North Carolina at Pembroke from 2014 to 2022.
Delta-v in feet per second, and fuel requirements for a typical Apollo Lunar Landing mission. In astrodynamics and aerospace, a delta-v budget is an estimate of the total change in velocity (delta-v) required for a space mission. It is calculated as the sum of the delta-v required to perform each propulsive maneuver needed during
Delta-v is typically provided by the thrust of a rocket engine, but can be created by other engines. The time-rate of change of delta-v is the magnitude of the acceleration caused by the engines, i.e., the thrust per total vehicle mass. The actual acceleration vector would be found by adding thrust per mass on to the gravity vector and the ...