A satellite orbits around the earth due to
A.Celestial force
B.Gravitational force
C.Centrifugal force
D.Centripetal force
E.All of the above
A.Celestial force
B.Gravitational force
C.Centrifugal force
D.Centripetal force
E.All of the above
A.tenacity
B.dustility
C.porosity
D.malleability
A.square
B.circular
C.rectangular
D.any of the above
A.Inward projecting entrances
B.Square bell mouth entrances
C.Circular bell mouth entrances
D.Slightly rounded entrance
E.Square cornered entrance
A.37.57 psi suction
B.10 psi suction
C.13.757 psi suction
D.23.757 psi suction
A.The first row
B.Row with maximum rivets
C.Middle row
D.End row with one rivet only
E.All rows have same strength
A.56.7 x 10-9
B.1.335 x 10-12
C.4.87 x 10-8
D.0.174 x 10-8
E.0.567 x 10-4
A.Engine cylinder diameter
B.B.H.P.
C.Speed
D.Mean effective pressure
E.Weight of engine
A.8 to 15 cfm/sq ft
B.0.2 to 0.5 cfm/sq ft
C.50 to 60 cfm/sq ft
D.0.01 to 0.1 cfm/sq ft
A.1 to 3 days
B.3 to 5 days
C.7 to 21 days
D.20 to 30 days