LUNASCAN MISSION REPORT:
Session
# 20151022 – 12 - 94
2. EPHEMERIS:
Observatory: +37°34' +87°32' Tz:
0h00m
Date: 2015-10-22 18:34:41
Date (TT): 2015-10-22 18:35:50
(J2000) Right Ascension:
21h41m49.96s
(J2000) Declination: -11°16'28.2"
(Date) Right Ascension:
21h42m41.28s
(Date) Declination: -11°11'58.8"
Distance: 371410Km
Apparent diameter: 32.17'
Colongitude: 30.4°
Phase: 65.3°
Lunation: 9.77 days
Illumination: 70.9%
Sub-solar latitude: 0.8°
Libration in Latitude: -03°17'
Libration in Longitude: -05°16'
Position angle: -20.4°
Azimuth +90°46'
Altitude -17°03'
Rise: 20h02m
Transit: 0h48m
Set: 6h20m
Rise azimuth: +103°16'
Transit Altitude: +41°
Set azimuth: +254°09'
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3. DETAILED ANALYSIS/NOTES:
18:34:00 Q start / no WWV carrier
18:35:34 Q Good ac trans
19:21:07 Q wwv on / good audio and video
19:59:50 EOM
18:34:00 Q aok but no wwv
19:21:00 Q wwv on
CABCAM good but no wwv
SSI CAM
00:01:35 el - target acq / no wwv
00:02:32 great copernicus
00:05:30 el ac trans
00:39:17 el improving conditions / great copernicus
00:45:00 el awesome copernicus / cap21
00:46:46 el wwv on
00:47:30 el = 0h20m cut
00:54:25 el great tycho
cap 23
01:25:00 eom
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4. EQUIPMENT MODE LEVEL
RECORDERS
VHS1 on
VHS2 on
VHS3 on
VHS 4 on LIMA 2 Skycam
(B Cam on
DVR1 on
DVR2 on
QUAD CAMERA POSITIONS:
All camera outputs to Quad SAMSUNG SCQ-041P
Camera 1 B-Cam - (SC-NVA5), wide angle
& A-Cam (SC-NVA5) 9x50 #51611 Celestron
finder w/crosshairs)
Y=video
R=power
Camera 2 CabCam
cam 1 (color, SC-NVA5 to Quad), cam 2 (Sony CL-34S-2T,
night vision, security, to Lab via
RG59)
Camera 3 VMA graphics/LPI not used
Camera 4: SSI/C-8. .
COMPUTERS:
PC1 System
Dell Intel Pentium 4 processor
2 Gigahertz, 256 meg
C Drive, 40 GB
D Drive, 111 GB
Digital to Analog Converter 2: TEP-100 Elite Pro II
Aperture video recorder DVR2
No graphics used
Feeding Quad Cam Position
4
PC2 System
VIRTUAL MOON ATLAS graphics left
Feeding Quad Cam Position 3
CAMERAS:
Camera 1
Celestron Neximage Solar System Imager
SSI or A camera = 2032/5=400x
No Barlow or focal reducer used
delivers simrange of 600 mi
and FOV of 400 miles
CCD sensor (Charge Coupled Device)
Type HAD (1/4")
OPTICS, prime focus 5 mm
Active area 3.6mm x 2.7 (4.5 mm diagonal)
Pixel size 5.6 micron, square
VGA resolution (640x480) color ¼” CCD chip
Maximum usable framerate @
640x480
(uncompressed): 30 fps
#11 yellow written filter
Compression 1420
?-Bit on-chip A/D converter
3 MP
Sensitivity <1 lux
ACOMP Computer
Camera 2
LPI (NOT UTILIZED THIS MISSION)
LPI or B camera = 2032/6=340x
Meade Lunar Planetary Imager
Type HV7131E1 (1/3")
OPTICS, prime focus. 6 mm.
Active area 5.18x3.90 mm (6.5 mm diagonal)
Pixel size 8.0 micron, square
VGA resolution (640x480) color
Max usable framerate @
640x480
(uncompressed): 36 fps
Compression 1420
8-Bit on-chip A/D converter
1.3 MP
Sensitivity <?lux
BCOMP Computer
Compaq Presario sr1218nx XP Home
2.67 GHZ processor, 760 mb
C Drive 80 GB hard drive
OPTICAL TUBE:
Celestron C-8 SCT 8” optical
tube
2032 mm f/l
F10
Resolution at lunar range = 0.68 /
.81086 mi or 4281.36469 feet
(30.19' X 60 = 1811.4" /.68' resol
= factor of 2663.82353
2160 miles / 2663.82353 = .81086 mi resolution)0.621 mi/km
1 m = 3.28 ‘
CONFIG:
(X) SSI in scope
back
( ) Diagonal and ( ) binoc viewer. Extended hand
control DOB Driver II