The document contains technical specifications for an aircraft, including a maximum speed of 850 km/h, range of 6500 km, maximum height of 12 km, and ability to carry up to 15 passengers. It also includes graphs of various aerodynamic parameters like lift and drag coefficients over mach number and altitude. Tables show thrust requirements and load distributions. Bending moment and shear force diagrams are presented. The second part of the document outlines manufacturing cost details for an unnamed system, listing material, equipment, labor, and other expenses totaling over $4 million. It includes a planned profit margin and calculations to determine wholesale price with value-added tax.

3. Vcr = 850 Km/h
Range = 6500 Km
Hcr = 12 Km
Passenger = upto 15

8. 6
5
4
3
2
1
0
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9
Cya,Cyamax
Mach
Cya0
Cya3
Cya6
Cya11
Cymax

9. SPEED OF LEVEL FLIGHT
WITH ALTITUDE
1.4
1.2
1
0.8
0.6
0.4
0.2
0
Polar Graph
0 0.05 0.1 0.15
Cya
Cxa
H=0
H=3
H=6
H=11
14
12
10
8
6
4
2
0
0 100 200 300
V cont
Vmin
Vmax
Vopt
Vmin.per

10. 200000
180000
160000
140000
120000
100000
80000
60000
40000
20000
0
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
Thrust (N)
Mach
Preq0
Preq3
Preq6
Preq11
Pavb0
Pavb3
Pavb6
Pavb11

12. 50
40
30
20
10
0
-10
-20
Distributed Load
0 0.2 0.4 0.6 0.8 1 1.2
qa,qf,qt
Z
qa,
qf
qt
30
20
10
0
-10
-20
-30
-40
-50
-60
-70
-80
-90
-100
-110
-120
-130
-140
-150
-160
-170
-180
-190
-200
-210
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 1.1
Qd,Qc,Qt
Z
Q­d
Qc
Qt
Graph of Shear force

13. 50
0
-50
-100
-150
-200
-250
-300
-350
-400
-450
-500
-550
-600
-650
-700
-750
-800
-850
Bending Moment
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 1.1
Mc,Md,Mtot
Z
Mc
Md
Mtot
100
50
0
-50
-100
-150
-200
-250
-300
-350
-400
-450
Reduced Moment
0 0.2 0.4 0.6 0.8 1 1.2
Mrc,Mrd,Mtot
Z
Mztot
Mrd
Mrc

25. S.No Articles
Expenses
(in million $)
1 Materials and Raw Materials
0.1986
2 Purchased devices , onboard equipments
1.741
3 Manufacturing Repair of special technological equipment
1.108
4 Wage
0.96
5 Indirect Shop expenses 0.416
6 Indirect Manufacturing expenses 0.298
7 Taxes 0.0252
8 Total ( Manufacturing expenses) 3.889
9 Outside Manufacturing expenses 0.1942
10 Total Manufacturing Cost Price 4.079
11 Profit (Planned) 0.612
12 Wholesale Price 4.6911
13 Value Added Tax 0.938
14 Wholesale Price with VAT 5.63

28. = 1438 lm (According to our work shop parameters )
SO we had chosen CFL bulbs as they had efficiency and low power consumption
We had recommended GE 23 watt which produce 1600 lm