Question Statement:
A satellite is injected at an altitude of 350 km above the Earth's surface, with a velocity of 8.0 km/s
parallel to the local horizon. (Earth radius=6378 km, µE (GM=Gravitational constant × Earth mass)
= 3.986×1014 m3s-2). The satellite
(A) forms a circular orbit. (B) forms an elliptic orbit.
(C) escapes from Earth's gravitational field. (D) falls back to earth.
END OF THE QUESTION PAPER
Q. No Type Section Key Marks
1 MCQ GA C 1
2 MCQ GA B 1
3 MCQ GA B 1
4 MCQ GA B 1
5 MCQ GA C 1
6 NAT GA 120.0 : 120.0 2
7 MCQ GA C 2
8 MCQ GA C 2
9 MCQ GA A 2
10 NAT GA 7.0 : 7.0 2
1 MCQ AE A 1
2 NAT AE -3.0 : -3.0 1
3 MCQ AE D 1
4 MCQ AE C 1
5 MCQ AE D 1
6 MCQ AE C 1
7 MCQ AE C 1
8 MCQ AE A 1
9 MCQ AE B 1
10 MCQ AE B 1
11 NAT AE 2.0 : 2.0 1
12 MCQ AE A 1
13 MCQ AE B 1
14 NAT AE 5.0 : 5.0 1
15 MCQ AE B 1
16 NAT AE 1.0 : 1.0 1
17 NAT AE 0.0 : 0.0 1
18 MCQ AE D 1
19 MCQ AE C 1
20 MCQ AE B 1
21 MCQ AE C 1
22 MCQ AE B 1
23 MCQ AE A 1
24 MCQ AE A 1
25 MCQ AE C 1
26 NAT AE 162 : 166 ; 1147.0 : 1150.0 2
27 MCQ AE B 2
28 NAT AE 2.9 : 3.1 2
29 MCQ AE D 2
30 NAT AE 40.0 : 41.0 2
31 MCQ AE B 2
32 MCQ AE B 2
33 NAT AE 1305 : 1305 2
34 MCQ AE B 2
35 MCQ AE A 2
36 MCQ AE A 2
37 NAT AE 5.0 : 5.0 2
38 NAT AE 1.5 : 1.7 2
39 MCQ AE B 2
40 NAT AE 2.4 : 2.6 2
41 NAT AE 0.99 : 1.01 2
42 NAT AE -11.0 : -11.0 2
43 NAT AE 3.13 : 3.15 2
44 NAT AE 0.56 : 0.58 2
45 NAT AE 548 : 550 2
46 NAT AE 310 : 315 2
47 MCQ AE C 2
48 NAT AE 7690 : 7710 2
49 NAT AE 8.6 : 8.7 2
50 NAT AE 25.0 : 25.0 2
51 MCQ AE D 2
52 MCQ AE C 2
53 NAT AE 20.0 : 21.0 2
54 MCQ AE C 2
55 MCQ AE B 2