Advances in Spacecraft Technologies Part 2 ppt
Advances in Spacecraft Technologies Part 2 ppt
... mission (Mori et al, 20 10; Normile, 20 10; Sawada et al, 20 10).
0
2
4
6
8
10
12
14
16
18
20
22
24
26
28
30
32
34
1000 10000 100000
Sail Assembly Loading (g m
-2
)
Sail Area (m
2
)
MeSR
IHP
JAtP
SbSR
SPO
Kuiper ... Dynamic and Control, Vol .2, No .2, Feb .20 04, pp. 38- 42 (in
Chinese)
Advances in Spacecraft Technologies
54
Garwin, R.L., Solar Sailing –...
Advances in Spacecraft Technologies Part 5 pptx
... Protection System (TPS) Tiles of Spacecraft
181
21 22
22
2
22
22
11
()
1
,
n
mp
hhy
AI
y
IA
η
ηη
⎫
=− − +
⎪
⎪
⎬
⎪
==
⎪
⎭
(25 )
22
22 2 122 2
22
22
22 2
1
11
()()()
2
1
()
2
n
m
hy hhhy
AI
hy
I
ζ
ζ
⎫
=+−+−
⎪
⎪
⎬
⎪
=−
⎪
⎭
... Advances in Spacecraft Technologies
1 62
1
1
()
11 1
()
2
11
1
2
(())()()
22 222 222 1 12
()
21 12
4
()
22 221
1
(())()()...
Advances in Spacecraft Technologies Part 13 ppt
... m
2
r2
2
+ m
3
r3
2
+ 2L
2
L
3
m
4
+ 2L
2
m
3
r
3
)
η
2
=(L
2
2
m
3
˙
θ
1
2
sin (2
2
)) /2 − (L
2
2
m
3
˙
θ
2
2
sin (2
2
)) /2
+(L
2
2
m
4
˙
θ
1
2
sin (2
2
)) /2 − (L
2
2
m
4
˙
θ
2
2
sin (2
2
)) /2
+(L
2
3
m
4
˙
θ
1
2
sin (2
2
)) /2 ... (L
2
2
m
4
˙
θ
2
2
sin (2
2
)) /2
+(L
2
3
m
4
˙
θ
1
2
sin (2
2
)) /2 +(L
2
3
m
4
˙
θ
3
2
sin...
Advances in Spacecraft Technologies Part 2 pdf
... Mini-Magnetospheric Plasma Propulsion
(M2P2): High Speed Propulsion Sailing the Solar Wind,” Proc. STAIF 20 00, M. S. El-
genk, ed. AIP 20 00.
Advances in Spacecraft Technologies
58
Sailing ... &
Casalino, 20 01; Dachwald, 20 04a, 20 04b, 20 05; Garner et al, 20 00, 20 01; Leipold & Wagner,
1998; Leipold, 1999; Leipold et al, 20 06, 20 10b; Lyngvi et al, 20...
Advances in Satellite Communications Part 2 pptx
... coating
non-loss EDT
lossy EDT
a)
1.8 1.9 2 2.1 2. 2 2. 3 2. 4 2. 5 2. 6 2. 7 2. 8
1.6
1.8
2
2 .2
2.4
2. 6
2. 8
3
3 .2
3.4
3.6
Frequency (GHz)
VSWR
pec
practical design
copper
lossy dielectric coating
non-loss ... is achieved with h/H = 0 .26 (Mimaki and
Nakano, 1998; Skiljo et al., 20 10).
1.8 1.9 2 2.1 2. 2 2. 3 2. 4 2. 5 2. 6 2. 7 2. 8
6
7
8
9
10
11
12...
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 ... February, 20 11
Printed in India
A free online edition of this book is available at www.intechopen.com
Additional hard copies can be obtained from orders@intechweb.org
Advances in...
Advances in Spacecraft Technologies Part 3 potx
... no .2,
20 07, 307-317.
Advances in Spacecraft Technologies
92
The centrifugal oil lubricator (Sathyan, et.al., 20 08) contains a reservoir cup and an inner
sleeve made of aluminum and machined ... 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...
Advances in Spacecraft Technologies Part 4 docx
... Margin Mass Margin Mass Margin Mass Margin
Thrust
misalignment
propellant mass
3 Kg 20 % 0 Kg 20 % 3 Kg 20 % 0 Kg 20 %
Solar pressure,
safe
manoeuvres
and initial
despin
1 Kg 20 % 1 Kg 20 % ... 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 y...
Advances in Spacecraft Technologies Part 6 pot
... written in
vector form as
[]
[]
T
123
T
12 13 21 23 31 32
λ = λλλ
δ = δδδδδδ
(13)
Part 2
Cutting Edge State Estimation Techniques
Advances in Spacecraft Technologies
22 2
estimates in ... detection index defined in Table 1.
Advances in Spacecraft Technologies
20 8
0 5 10 15
-20
-10
0
10
20
J
11
0 5 10 15
-20
-10
0
10
20
J
22
0 5...
Advances in Spacecraft Technologies Part 7 docx
... the inverse metric g
μν
eff
g
eff
να
= δ
μ
α
,
the covariant form of the effective metric then reads
g
eff
μν
= g
μν
−
2B
2
/b
2
(2B
2
/b
2
+ 1)
V
μ
V
ν
+
2B
2
/b
2
(2B
2
/b
2
+ 1)
l
μ
l
ν
, (28 )
which ... obtain
g
μν
eff
=
1
+
F
b
2
g
μν
−
2B
2
b
2
[
h
μν
+ l
μ
l
ν
]
. (24 )
Then, by noting that
F
= F
μν
F
μν
= 2( E
2
− B
2
) , (25 )
23 9
Nonlinear Electrodyna...
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