To get rockets into orbit, they need much more thrust than the amount that will get them up to the required altitude. They also need sufficient thrust to allow them to travel with very high orbital speed. ... If speed is less than this, an object will fall back to the Earth
Answer:
maximum isolator stiffness k =1764 kN-m
Explanation:
mean speed of rotation ![=\frac{N_1 +N_2}{2}](https://tex.z-dn.net/?f=%3D%5Cfrac%7BN_1%20%2BN_2%7D%7B2%7D)
![Nm = \frac{500+750}{2} = 625 rpm](https://tex.z-dn.net/?f=Nm%20%3D%20%5Cfrac%7B500%2B750%7D%7B2%7D%20%3D%20625%20rpm)
![w =\frac{2\pi Nm}{60}](https://tex.z-dn.net/?f=w%20%3D%5Cfrac%7B2%5Cpi%20Nm%7D%7B60%7D)
=65.44 rad/sec
![F_T = mw^2 e](https://tex.z-dn.net/?f=F_T%20%3D%20mw%5E2%20e)
![F_T = mew^2](https://tex.z-dn.net/?f=F_T%20%3D%20mew%5E2)
= 0.1*(65.44)^2
F_T =428.36 N
Transmission ratio ![=\frac{300}{428.36} = 0.7](https://tex.z-dn.net/?f=%3D%5Cfrac%7B300%7D%7B428.36%7D%20%3D%200.7)
also
transmission ratio ![= \frac{1}{[\frac{w}{w_n}]^{2} -1}](https://tex.z-dn.net/?f=%3D%20%5Cfrac%7B1%7D%7B%5B%5Cfrac%7Bw%7D%7Bw_n%7D%5D%5E%7B2%7D%20-1%7D)
![0.7 =\frac{1}{[\frac{65.44}{w_n}]^2 -1}](https://tex.z-dn.net/?f=0.7%20%3D%5Cfrac%7B1%7D%7B%5B%5Cfrac%7B65.44%7D%7Bw_n%7D%5D%5E2%20-1%7D)
SOLVING FOR Wn
Wn = 42 rad/sec
![Wn = \sqrt {\frac{k}{m}](https://tex.z-dn.net/?f=Wn%20%3D%20%5Csqrt%20%7B%5Cfrac%7Bk%7D%7Bm%7D)
k = m*W^2_n
k = 1000*42^2 = 1764 kN-m
k =1764 kN-m
Answer:
2.379m
Explanation:
The width = 23m
The depth = 3m
The radius is denoted as R
The wetted area is = A
The perimeter perimeter = P
Hydraulic radius
R = A/P
The area of a rectangular channel
= Width multiplied by Depth
A = 23x3
A = 69m²
Perimeter = (2x3)+23
P = 6+23
P= 29
Hydraulic radius R = 69/29
= 2.379m
This answers the question
Thank you!
Answer:
porosity = 0.07 or 7%
dry bulk density = 3.25g/cm3]
water content =
Explanation:
bulk density = dry Mass / volume of sample
dry mass = 0.490kg = 490g
volume = πr2h = 3.142 * 2 *2 *12 = 150.8cm3
density = 490/150.8 = 3.25g/cm3
porosity =
=
= 0.07 or 7%
water content =
= 7%
Answer:
(absolute).
Explanation:
Given that
Pressure ratio r
r=8
![r=\dfrac{P_2_{abs}}{P_1_{abs}}](https://tex.z-dn.net/?f=r%3D%5Cdfrac%7BP_2_%7Babs%7D%7D%7BP_1_%7Babs%7D%7D)
-----1
P₁(gauge) = 5.5 psig
We know that
Absolute pressure = Atmospheric pressure + Gauge pressure
Given that
Atmospheric pressure = 14.5 lbf/in²
P₁(abs) = 14.5 + 5.5 psia
P₁(abs) =20 psia
Now by putting the values in the above equation 1
Therefore the exit gas pressure will be 160 psia (absolute).