Advances in Spacecraft Technologies Part 5 pptx
Advances in Spacecraft Technologies Part 5 pptx
... determined as follows.
If the plane of i-facet of Sc does not cross the planet:
4
cos 1 sin
1
23
( ) (1 sin 2 sin ln );
2
4 2 sin 1 sin
22
cos (3 sin ) 1 sin
() ln
3
16 sin 1 sin
2
(1 sin ) ... (84)
1234
0
llll
eA e A eA e A
μμνν
μμ νν
−−
−
+− =
( 85)
Inserting (67) and (69) into (51 ) and then inserting the obtained results into (78)~(81), we
have
1234
BBBB DP+++=− (86)
1234
0B...
Advances in Optical Amplifiers Part 5 pptx
... shown in Fig .5 as inset (ii).
154 0.0 154 2 .5 154 5.0 154 7 .5 155 0.0 155 2 .5
-50
-40
-30
-20
-10
0
Optical power (dBm)
Wavelength (nm)
1.25nm/D
Converted
signal
17dBm
154 3 .5 154 5.0 154 6 .5 154 8.0 154 9.
5
-60
- 45
-30
- 15
0
Optical ...
10Gb/s
TDS-684
AWG
154 2.0 154 3 .5 154 5.0 154 6 .5 154 8.0
-50
-40
-30
-20
-10
0
Optical power (dBm)
Wavelength (nm)
0.75nm...
Advances in Spacecraft Technologies Part 1 doc
... re-emerging
troubles of actual spacecraft docking to help finding solution, checking the initial docking
conditions of spacecraft docking process, testing the action and counteraction of spacecraft ... scale to docking/berthing hardware as the physical model participating in the
simulation.
Advances in Spacecraft Technologies
Edited by Jason Hall
Published by InTech
Janeza...
Advances in Spacecraft Technologies Part 2 ppt
...
feeding cables were relayed by coaxial connectors penetrating the wall.
Advances in Spacecraft Technologies
66
3 456 7891011
-60
-50
-40
-30
-20
-10
Frequency [GHz]
Propagation gain [dB]
3 456 7891011
-50
-40
-30
-20
-10
0
Frequency ... 200700320 65.
Advances in Spacecraft Technologies
56
Lyngvi, A., Falkner, P., Peacock, A., The Interstellar Heliopause Probe...
Advances in Spacecraft Technologies Part 3 potx
... designs of bearing units available such as rotating shaft design and
rotating housing design. In rotating shaft design, the bearing housing is rigidly mounted on
Advances in Spacecraft Technologies ... rotating housing bearing
unit used in a momentum wheel.
In bearing units, ball bearings with non-metallic retainers [cages] are generally used.
However, retainerless bearings...
Advances in Spacecraft Technologies Part 4 docx
... (days)
0 5 10 15 20
Heat Flow (µW/g)
0
10
20
30
40
50
60
70
ADN/GAP, FP09 053
Acceptance limit at 75 C according to STANAG 458 2
Fig. 7. Thermal stability at 75 °C of ADN/GAP propellant containing ... bonded grains were cast in steel cartridges as shown in Fig. 9. A liner based on HTPB
was used. Some minor machining was needed after casting. The propellant was easy to
machine...
Advances in Spacecraft Technologies Part 6 pot
... detection index defined in Table 1.
Advances in Spacecraft Technologies
208
0 5 10 15
-20
-10
0
10
20
J
11
0 5 10 15
-20
-10
0
10
20
J
22
0 5 10 15
-20
-10
0
10
20
J
33
0 5 10 15
-20
-10
0
10
20
J
12
0 ... estimation error
0 5 10 15
-0.01
-0.0 05
0
0.0 05
0.01
MIS
0 5 10 15
-1
-0 .5
0
0 .5
1
x 10
-3
Bias
Time (min)
Fig. 7. Rate sensor calibration er...
Advances in Spacecraft Technologies Part 7 docx
...
4
5
6
7
8
9
1.600 - 1.700
2.1 45 - 2.1 85
2.1 85 - 2.2 25
2.2 35 - 2.2 85
2.2 95 - 2.3 65
2.360 - 2.430
30 m
TIR
10
11
12
13
14
8.1 25 -8.4 75
8.4 75 - 8.8 25
8.9 25 - 9.2 75
10. 25 ... 100 150 200 250
-0. 05
0
0. 05
Error
time, sec
gyroscope
0 50 100 150 200 250
-1
0
1
time, sec
star tracker 1
0 50 100 150 200 250
-0.02
0
0.02
time, sec
s...
Advances in Spacecraft Technologies Part 8 pdf
...
8
s
M
=
.
- 35 -30 - 25 -20 - 15 -10 -5 0 5 10
χ/λ
1
-5
0
5
10
15
20
25
30
35
40
45
50
55
60
65
70
75
80
85
90
95
100
1 05
110
1 15
q
x
M
s
=3.8
M
s
=9
M
s
=10
- 35 -30 - 25 -20 - 15 -10 -5 0 5 10
χ/λ
1
-1
0
1
2
3
4
5
6
7
8
9
10
11
12
13
τ
χχ
M
s
=3.8
M
s
=9
M
s
=10
... 21
×
× in the
physical space.
0 50 0 1000 150 0 2000 250 0 3000 350 0 40...
Advances in Spacecraft Technologies Part 9 pot
... 0.1616 0.4827 1. 653 2 8.2 659
Re
∞
e
3943.13 2782 .54 1649.69 2 45. 32 131.11 27.07 7.90 1 .58
()Hkm
f
58 .07 60.96 65. 44 62.01 61. 45 65. 55 75. 07 84.79
a Diameter of sphere in meters. b Mach ... 13 25- 1336.
Advances in Spacecraft Technologies
338
DSMC 0 DSMC 25 DSMC 50 Experiment
Average 2.096182 2.089747 2.083312 2.10 454 39
Max 2.202087 2.698921 3.1 957...
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