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author | prashantsinalkar | 2017-10-10 12:27:19 +0530 |
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committer | prashantsinalkar | 2017-10-10 12:27:19 +0530 |
commit | 7f60ea012dd2524dae921a2a35adbf7ef21f2bb6 (patch) | |
tree | dbb9e3ddb5fc829e7c5c7e6be99b2c4ba356132c /3720/CH6/EX6.6 | |
parent | b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b (diff) | |
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initial commit / add all books
Diffstat (limited to '3720/CH6/EX6.6')
-rw-r--r-- | 3720/CH6/EX6.6/Ex6_6.sce | 18 |
1 files changed, 18 insertions, 0 deletions
diff --git a/3720/CH6/EX6.6/Ex6_6.sce b/3720/CH6/EX6.6/Ex6_6.sce new file mode 100644 index 000000000..75d1af7dc --- /dev/null +++ b/3720/CH6/EX6.6/Ex6_6.sce @@ -0,0 +1,18 @@ +//Example 6_6
+clc;clear;
+// Given values
+m_f=100;// kg
+V_f=3000;//Velocity of solid fuel in m/s
+dt=2;// seconds
+m_sat=5000;// kg
+
+// Calculation
+//(a)
+a_sat=((m_f/dt)*V_f)/m_sat;
+printf("The acceleration of the satellite during the first 2 s=%0.0f m/s^2\n",a_sat);
+//(b)
+dV_sat=a_sat*dt;
+printf("The change of velocity of the satellite=%0.0f m/s\n",dV_sat);
+//(c)
+F_sat=(0-(m_f/dt)*(-V_f))/1000;
+printf("The thrust exerted on the satellite=%0.0f kN\n",F_sat);
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