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予稿集 p.124-125
P- 37 !"#$%&'()*+,-./012 Initial results of the Laser Altimeter onboard KAGUYA (SELENE) !"#$%&'()%*!+,%-./0%1*23%45'6 Seiichi Tazawa, Hiroshi Araki, Hirotomo Noda, Nobuyuki Kawano, Sho Sasaki 789:;<=>? @ABCD National Institutes of Natural Sciences, National Astronomical Observatory of Japan EFGH%I!J Teiji Kase, Shigeru Murata KLMNOPQR NEC Corporation ABSTRACT The Laser Altimeter is one of the instruments on board KAGUYA (SELENE) main orbiter, and measures the distance from the main orbiter to the lunar surface. KAGUYA was launched by the H-IIA F13 Launch Vehicle at 10:31:01 a.m. on September 14, 2007 (JST) from the Tanegashima Space Center. The LALT measured the altitude on November 25 for the first time after sensitivity adjustment of receiver system. The LALT started nominal observation on December 30, 2007. We will report the performance of the hardware and the status of data acquisition. 1. d•^ƒVødµ|ùúû“t”›\üò%cde STUV WXYZ;<[\=>]^_`abcdefg hSELENEiS 2007 j 9 ^ 14 K 10 k 31 l 01 mV nopWXqrstuv H-IIA wxyz 13 {=V| }~•€•‚%^ƒ•„…† 100km%‡ˆ‰Š‹ 90 …]‡ˆVŒ•Ž‚•• cdefgV‘’Ž‚•“t ”„…•hLALT–Laser AltimeteriScdefgd •^ƒ—˜]™šh„…i›œ•žŸ ¡˜¢v% @ABCD RISE ^£¤¥w¦§¨z©ª«V=¬ -®¯u°±ts²³›´µ|¶Ÿ• LALT ]·¸¹ºS%1i^]»¼]„½…¾•% 2i¿À›ÁÂ^ƒÃÄÀ˜]Å»„…Æ]ÇÈ%3i oabc¯ÉÊgËc¯ÌÊg›Íµ•^ÎÏУ¤ fgÕ^ƒê]™š›œ•žŸ ¡˜¢v%ab> ýÙÚ]þÿÚhLALT-EiÕab>ý!Ú]+Z ƒ h"V^›Â¶|¶Ÿ#iV$%ï&•‚•“t” '()ÚhLALT-TRi]*Ü]+r,t-rz˜> ÈŽ‚|¶Ÿ•ùúû“t”S Nd:YAG “t”›. ®ò%ùúû/ 17nsec%ùúû0-ú1t100mJ% 2v3ò4…éHz ˜¢Ÿ•')5t6]78/S 0.4mrad ˜¢v%9: 73mm ];<“=P>?@A B›Cò')Ž‚Ÿ•()S9: 100mm ]DqE “rPFü@AB›®¶%Si-APD ˜()žŸ•() G*S 1mrad ˜¢Ÿ•Figure 1 VcdefgÕ>ý Vßvï¶|¶Ÿ LALT ›Hž• ÑyÒÓrhRSAT/VRADid•Ô•‚ŸÎÏб tsÕÖ×Ø•%^ÙÚ>ÛVܶ|]ÝÞßÔ˜ ¢Ÿ•^ƒ]à… 75 …á•]¿À]„…±ts›ß ÔžŸ]Scdefg] LALT ©âU|˜¢v%¿ ÅÀ]„½…„…Æ]ÇÈVθÊãä›å•žæ Õ©ç莂|¶Ÿ•ÑyÒÓréjê]•œëê LALT ]ì홚Sîˆï𘆠2km%¿ï𘆠100m ›ñ•ò|¶Ÿ•LÞó˜Scdefg}~•€ô V´µ• LALT ]âç-®õåVöò|Þ󞟕 2. JAXA/SELENE “t”„…•÷¸ LALT S^_`‡ˆ•›-´žŸ·abcdefg - 124 - Figure 1 The LALT onboard SELENE 3. ‡ˆ•âç-®õå ‡ˆ•˜SI`Vl&|=JKLMN›´µ•• Table 1 V‡ˆ•˜´µ•âç=JKL$O›Hž• LALT S 2007 j 9 ^ 23 KV^PQ‡ˆ•˜}~• €ôSTU|MR›Œ•ò%SÚMT%MU%V…% Wtsþÿ=J]XÃY›KLò•hZý[T=J KLi •2007 j 11 ^ 1 KV^_`‡ˆ•˜\Ì$… Zý[T=JKL›´µ•ô%2007 j 11 ^ 24]25 KVZý„T=JKL›´¶%“t”\^®]„T MR%“t”\ü=J%¯u°œ™=J©_"˜¢ lon: 63.0 W ŸæÕ›KLò••„TMR]`TSaMVbcò Ê©•dKá•d& 0V d• 2.5kVhe,fÏMTi lon: 60.9 W !"#$%&$#'&()$#*+$%,&-#.+/+"+* 0++12334445)1/5".%$5*'"3%*.6"%7*.38$17$+$)693 —˜g5V`Tò•• „T=JKLk]cdefg]‡ˆ› Figure 2 V% Figure 2 œ™=JKL˜ßÔò•±ts› Figure 3 VHž• Trajectory of the KAGUYA main orbiter over the Pythagoras crater hKcdefgSisjkû¨“tsh63.5N, 63.0W ïði•Z›Cv%l… 60.9mW ]œ™˜S¨“t sÙÚ]ìnÊÚl›Cµ|¶Ÿ©%† 4 kêô] l… 63.0mW ]œ™˜Sªop]„…¥wqrsú ›ßÔžŸt©fu••ªopŠƒ]‰ŠS±ts d•† 25 …˜¢v%„…† 100km ˜ 25 …—˜]v ʉŠÅ]œ•\wJ˜¢ŸæÕ›xyžŸ±ts ›ßÔò••—•hK]œ™Èz{S 98.6%hÒÓ yzI 8004 V|ò%œ™ÈzI 7892i˜¢v%„ ¶K{˜±ts›ßԘɟæÕ©˜É•• Table 1 Initial check out of the LALT Date Ù} ~• 2007/9/14 def}•€ MR OFF Zý[T=JKL [TMR h^PQ‡ˆ•i WtsKL Zý[T=JKL [TMR h^_`‡ˆ•i WtsKL 2007/9/23 2007/11/1 2007/11/24, 25 2007/12/11, 12 2007/12/21 Zý„T=JKL €rwt±•rE ‚ÖƒÇKL „TMR “t”KL Ã=¬ ON Figure 3 def•"-®[„ Topographic profiles of the Pythagoras crater 4. —ÕU ‡ˆ•˜“t”„…•]âç=JKL›´¶%ƒ Ç%=JV…†Ê¶æÕ%„…±tsVöò|„4 …˜±ts‡Ô©wJ˜¢ŸæÕ›KL˜É•• cd efgSˆ‰%†djê] Extend ÑyÒÓrVø& •Š‹Œ•©Ž•˜¶Ÿ• - 125 -