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1 50cm 2500mm 300mm 15 CCD

2 3

3 4

4 23 SORA Kwak SeungJo ˆ 300mm 2500mm ˆ WASP 1: CCD 200mm WASP cm 1

5 1: CCD 2: 1.4 MOST MOST mm,.. CCD KAI pixcel CCD () mm 9 9 μm A/D 16bit(65536 ) mm 730 g 2: CCD (KAI11000) electrons (500nm) 50 % 66 db 800 e/p/s 10 electrons ,,, CCD. CCD BS-43L. 1, FGK

6 CCD h, f θ h = f tan θ (4) 3.8μm., CCD,..,,, (),,. AD, D, f, λ(500nm), AD =2.44λ f =10.16μm (5) D, m,, p. p = m/2.5 (1), 15, p = 11000[photon/s m 2 ] (2). S N p Q t S = N P Qt (3), ,CCD..,, CCD CCD,.. CCD,,,.,.CCD,,.,.,,, SN. (N ph ), N ph = N P Qt (6) (N r ) CCD 3

7 3: SN SN CCD 6, 90, 540., 540[] 16bit 24bit = 25920byte 25kb (10),. 10e. SN CCD. = (N 2 r + N 2 ph ) (7) 2, SN 3. L,ΔL,S,N ()( ) < ()( ) (11) ΔL L > N S (8) ,, A/D CCD AD 16bit, , 10,., 2 10, electrons. 1e /count,1e ,1100,16bit byte = 2200 byte 20Mb (9) 20Mb.,, mm 4

8 H 0 ρ 0 ) ρ = ρ 0 exp ( hh0 (13) lnρ =lnρ 0 h (14) H : : mm 1800 mm mm 1200 mm ˆ ˆ ˆ ˆ a drag = 1 2 ρv2 SC d m (12) v S C D m ρ 5 4: H 0 =70.92[km] (15) ρ 0 = [kg/m 3 ] (16) IADC 2000km km ISS 30[deg]

9 : 5 5: a 6921 km h 550 km e 0 - i 30 deg Ω 0 deg cm 2500mm CCD CFRP CFRP 6 6

10 6: CFRP kgf/mm kgf/mm kgf/mm kgf/mm / C 4 5 Kcal/(m h C) Ω cm 6: 8: AR46AA-H100 7: 7 4 AR46AA-H CFRP 1 10 MLI MLI CCD 7: AR46AA-H100 5 N m kg m / 5 N m 11 N m 0 35 r/min 7

11 9: 11: MST-TA1202XD 8: MST-TA1202XD x V μm 0.25 mm/s 0.1 μm 1 μm 4000 g 8 N 220 g 10: MST-TA1202XD MST-TA1202XD 1 3 x,y,z 1μm 12mm MST-TA1202XD ˆ ˆ θ t [deg] d CCD f θ t = d f 180 π (17) CCD [mm] CCD mm mm 2500mm [mm] Δx CCD 8

12 12: 13: Δx ΔS mm ( ΔS = R 2 π 1 2 ( )) ( ) Δx Δx π cos 1 + Rx sin 1 (18) 2R 2R % % (18) 0.470[mm] 287[K] 304[K] 17[K] / C x[mm] 13 θ s ΔL x = αlδt = = (20) r θ s = 1 ( tan 1 2L 2r +tan 1 2 f f ( ) sin 1 r cos 1 2r tan f f L2 (19) ΔL CCD [mm] θ smax 19 θ smax =0.0287[deg] [mm] 9 9: mm 4 3DCAD Autodesk Inventor [N m] [N m] [N] [mm] [mm] 9 9

13 15: 14: MLI : JAXA PAF-239M 50[cm 3 ] 50[kg]

14 18: 17: 11: 10: x[mm] y[mm] z[mm] [kg] M 32 I xx [kgm 2 ] I yy [kgm 2 ] I zz [kgm 2 ] I xy [kgm 2 ] I xz [kgm 2 ] I yz [kgm 2 ] Dyneema Al A2024-T3 0.5 mm Al 1/ mm Al A7075-T H-IIA H-IIA DCAD Autodesk Inventor [Hz] : 11

15 12: A2024-T3 A7075-T kg/m GPa GPa MPa MPa 13: H-IIA 30Hz 4.0G 10Hz 1.8G Al 1/ kg/m GPa 2.4 MPa 2.7 MPa 21: 3.8 GPS 20: [MPa] A2024-T3 269[MPa] MS GPS GPS SpaceLink IGPS-1 14 MS = σ cr σ 269 1= (21) 6.74 MS : 12

16 23: 13

17 : GPS 7 m ±15 m 230 g mm 1.0 V 5.0 W AXELSPACE AxelStar SYSTRON DONNER QRS116 QRS : 100 deg/s deg/s φ mm 60 g 0.1 W 40m : (yaw/pitch) 7 arcsec (roll) 77 arcsec 8 8 deg 2,1,0.5,0.2 Hz deg/s 35 deg 516 g mm V 2.5 W : AXELSPACE AxelSun : 3 2 Honeywell HMR

18 17: 1 deg deg 46 g mm 5 V W I ω = ω (Iω + h RW ) ḣrw + T c (22) I : ω : h RW : T c : 26: ˆ ˆ 27: ˆ ˆ RW 18: 3.75 g mm 8 Hz 5 V 15 ma ±2 gauss 1 deg 0.1 deg T a = r F a r F a F a F a = 1 2 ρv2 C d A 15

19 ρ : = [kg/m 3 ] A : x y z A x =0.33[m 2 ] A y =0.54[m 2 ] A z =0.58[m 2 ] v : =7.5[km/s 2 ] C d : =2.0 r : r x =0.43[m] r y =0.43[m] r z =0.02[m] T a = [Nm] (23) : x [Nm] y [Nm] z [Nm] I u T g = 3μ I z I y θ ex R 3 I z I x θ ey 0 T sp = P s (1 + q)cosil s A P s : = [N/m 2 ] L s : r x =0.43[m] r y =0.43[m] r z =0.02[m] i : = 0[rad] q : = T sp = [Nm] (24) T g = 3μ R3u Iu R : = 6928[km] θ : = π/4[rad] T g = [Nm] (25) 0 T m = m B m : =0.2[Am 2 ] B : = [T] T m = [Nm] 19 16

20 3.9.3 RW RW RW 1[Nms] VECTRONIC Aerospace RW-VRW1 20: RW-VRW1 1.8 kg mm kgm 2 25 W ±5000 rpm 1.0 Nms M t = =2.08[AM2 ] (27) Surrey Satellite Technokogy Magnetorquer-MTR-5 21: 500 g mm kgm W ±5000 rpm 5.0 Am 2 29: 28: T = M B (26) M : B : 550[km] [T] RW [Nm] 45 ḣ RW = k d (ω d ω)+k p V (q q d ) ω d : [rad/s] ω : [rad/s] q : q d : ( ) : V ( ) : k p : k d :

21 30: : RW 32: 50 RW RW RW APC RW 24: Panasonic - NCA (11 2 ) 8.08 Ah V km BUS BUS BUS BUS BUS BUS 35-55[V] BUS 18

22 22: P 138 W P c - W P BAT - W η BAT X rad SA (2 ) X radv SA (2 ) V d V V e 39.6 V T d h T e h C 8.08 Ah DOD - % 23: Planet - GaAs ( ) V : BUS PPT BUS BUS BUS BUS BUS BUS BUS 19

23 25: 5V DC/DC Murata Power Solutions - UQQ-5/20-Q48-C - 48 V 75 V 18 V 5 V 20 A 100 W 91 % : 5V DC/DC 26: 12V DC/DC Murata Power Solutions - SPM D48-48 V 75 V 36 V 12 V 2.1 A 25.2 W 87 % 34: 5V 12V DC/DC 2 DC/DC V DC/DC 25, 35, 12V DC/DC : 12V DC/DC 20

24 1[deg] 1[deg] 27: Planet GaAs TJ 3.6 V 4.04 A 4.17 V 5.85 A 29.1 % mm 37: 47.9[V] 47.9[V] V SA, V BAT V LOSS =1.5[V] V SA V BAT + V LOSS =49.4[V] (28) V SA V mp N V SA = V mp N (29) T SA T SA,V mp V mp =(1 X radv )(Ṽmp + α v ΔT SA ) (30) X radv 2 ΔT SA α v V mp Ṽ mp =2.3[V],α v = [V/K] (31) [V] 5.16[V] P sa =(P e T e /X e + P m T m /X m + P d T d /X d )/T d (32) P, T, X e, m, d M P =(1 X rad )(M 24) (V mp + α v ΔT SA ) (I mp + α i ΔT SA ) (33) X rad,i mp,α i 2 I mp I mp =0.45,α i = [A/K] (34) P sa =93.6 M = P = 139[W] [cm 2 ] 4608[cm 2 ] ,

25 264 28: Panasonic NCA ( 1 ) 3.6 V 4.35 V (min) 4.04 Ah (typ.) 4.17 Ah 5.85 mm 60 mm 80 mm 67 g 38: [h] DOD 39DOD < 40% 40: : DOD Panasoic BUS 11 Panasonic NCA , z y 2 2 z x,y x,y 22

26 44: x 41: x y,z 45[deg] z 45[deg] 75[deg] y 1, 1 45: x () B e e B e = P ce T e η Line η DC/DC V e (35) () B d d B d = (P P cd)t d η BAT V d (36) 42: z (35),(36) DOD DOD = 1 C ( Be B d ) (37) (37) DOD : z 2 41 DOD 1 DOD 14.0% 1 DOD DOD < 40% 23

27 29: 550 km h h h 35.7 % 64.3 % h% RW h h 127 W 8.08 Ah BUS () 47.9 V BUS () 39.6 V η Line DC/DC 1η DC/DC 91 % DC/DC 2η DC/DC 87 % 2 1 DOD 28.0% DOD : Wh Wh Wh Wh 163[Wh] ˆ HK ˆ ˆ 0.1MB 30 = = 28[kbps] (38) 46: ˆ CCD CCD 1 20MB

28 [MB] HK 50[byte] 2[Hz] 1 HK 8.5[MB] (39) = =3.2[Mbps] (39) [Mbps] ˆ = 4 π 2 (40) 31: - 1 m S - 10 W K K ˆ S QPSK ˆ SURREY S S SpaceQuest S : GHz kg mm kbps C V W ˆ km 395 HK 47: S 25

29 48: S HK : S???? 3[dB] S (PFD) 5 154[dBW/4kHz/m 2 ] [dBW/4kHz/m 2 ]?? : S SEMC5701B CPU VR5701A JAXA HK : CPU HK 26

30 33: UPLINK DOWNLINK MHz mm 5 5 deg km EIRP dbw dbw 0 0 db dbi 0 0 db 0 0 db db 0 0 db db 0 0 db G/T db/k 0 0 db dbi 0 0 db dbk C/No dbhz db db db dbhz Eb/No db C/No dbhz db PFD( =5deg) dbw/4khz/m 2 PFD( =90deg) dbw/4khz/m 2 27

31 34: CPU mm 5 V 16 MB I/F USB1.1 CF Space Wire n i m i : i c pi : i T i,t j : i, j Q i : i C ij : i, j R ij : i, j σ : Q i = Q 1i + Q 2i + Q 3i + P i (42) Q 1i : Q 2i : Q 3i : P i : i C ij = h ij A ij (43) A ij : i, j h i j : i, j (44) R ij = ɛ i ɛ j F ij A i (45) ɛ i,ɛ j = i, j F i j : i j (46) F ij F ij = 1 cos θ i cos θ j πa i A i A j rij 2 da i da j (47) θ i : i, j A i,a j r ij : i, j (48) m i c pi dt i dt = Q i n n C ij (T i T j ) R ij σ ( Ti 4 j=1 j=1 Tj 4 ) (41) 52: 1 28

32 F F = R 2 e 1 (R e + H) 2 (51) R e : (6378[km]) μ : (700[km]) Q 3 53: Q 1 S [W/m 2 ] 1309[W/m 2 ] Q 1 Q 1 = S 1 Aμ (49) A : μ : θ μ =/ =cosθ Q 2 S 2 264[W/m 2 ] 140[W/m 2 ] Q 2 = S 2 AF (50) Q 3 Q 3 = αs 1 AF (52) α α = (+0.30, 00.15) ± ,16 1,13,15,16,17 CCD 14, K 29

33 35: [ ] [W] 3 RW RW RW : : [ ] [ ] H-IIA

34 54: 5 [10] [11] FB No [1] [2] 26 [3] [4] SPACE TELESCOPE SCIENCE INSTITUTE [5] SuperWASP [6] [7] Vol.16 No [8] Vol.41 No [9] ()

64 3 g=9.85 m/s 2 g=9.791 m/s 2 36, km ( ) 1 () 2 () m/s : : a) b) kg/m kg/m k

64 3 g=9.85 m/s 2 g=9.791 m/s 2 36, km ( ) 1 () 2 () m/s : : a) b) kg/m kg/m k 63 3 Section 3.1 g 3.1 3.1: : 64 3 g=9.85 m/s 2 g=9.791 m/s 2 36, km ( ) 1 () 2 () 3 9.8 m/s 2 3.2 3.2: : a) b) 5 15 4 1 1. 1 3 14. 1 3 kg/m 3 2 3.3 1 3 5.8 1 3 kg/m 3 3 2.65 1 3 kg/m 3 4 6 m 3.1. 65 5

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