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Exercise- -Load factor The picture shows the launch state of a missile sliding along the guide rail under the action of thrust P. It is known that the thrust P=450800N, the weight of the missile is G=20000N, the front leg A is a slider, the sliding friction coefficient is considered, and the rear leg B is a roller, ignoring the rolling friction. The launch angle is 0, try to use the above three expressions to calculate the load factor in the X and Y directions. R+RG cos B R₁₁ = Gl₂ ⋅ cos 0 |R₁f=F₁ e1 8. RB h Ꭱ . | RA R₁ = 1½-½ G cose 4 RB 1₁-12 Geose 1. y Sax = ? {a₁ = ? F₁-Gf cos

Exercise- -Load factor The picture shows the launch state of a missile sliding along the guide rail under the action of thrust P. It is known that the thrust P=450800N, the weight of the missile is G=20000N, the front leg A is a slider, the sliding friction coefficient is considered, and the rear leg B is a roller, ignoring the rolling friction. The launch angle is 0, try to use the above three expressions to calculate the load factor in the X and Y directions. R+RG cos B R₁₁ = Gl₂ ⋅ cos 0 |R₁f=F₁ e1 8. RB h Ꭱ . | RA R₁ = 1½-½ G cose 4 RB 1₁-12 Geose 1. y Sax = ? {a₁ = ? F₁-Gf cos

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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Exercise- -Load factor The picture shows the launch state of a missile sliding along the guide rail under the action of thrust P. It is known that the thrust P=450800N, the weight of the missile is G=20000N, the front leg A is a slider, the sliding friction coefficient is considered, and the rear leg B is a roller, ignoring the rolling friction. The launch angle is 0, try to use the above three expressions to calculate the load factor in the X and Y directions. R+RG cos B R₁₁ = Gl₂ ⋅ cos 0 |R₁f=F₁ e1 8. RB h Ꭱ . | RA R₁ = 1½-½ G cose 4 RB 1₁-12 Geose 1. y Sax = ? {a₁ = ? F₁-Gf cos
Transcribed Image Text:Exercise- -Load factor The picture shows the launch state of a missile sliding along the guide rail under the action of thrust P. It is known that the thrust P=450800N, the weight of the missile is G=20000N, the front leg A is a slider, the sliding friction coefficient is considered, and the rear leg B is a roller, ignoring the rolling friction. The launch angle is 0, try to use the above three expressions to calculate the load factor in the X and Y directions. R+RG cos B R₁₁ = Gl₂ ⋅ cos 0 |R₁f=F₁ e1 8. RB h Ꭱ . | RA R₁ = 1½-½ G cose 4 RB 1₁-12 Geose 1. y Sax = ? {a₁ = ? F₁-Gf cos
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