LUNASCAN
DATE-TIME: August 31. 2014 |
Routine Primary Targets: Theophilus, Mare Crisium |
Colongitude:
192.1° |
SYNOPSIS: EOM 1m31s elapsed or
|
1.
PRELIMINARY
QUAD
Durat = 1h31m45s
Good WWV
0h20m
CUT = 20:13:09 Target Acq
20:13:54 time fix 01h14m CUT
20:55:05 EOM
Q-SELECT
AOK
Good WWV
SKYCAM/METEOR
AOK
Good WWV
CABCAM
AOK
Good WWV
2. EPHEMERIS DE421
Observatory:
Date:
Date (TT):
(J2000) Right Ascension:
(J2000) Declination:
(Date) Right Ascension:
(Date) Declination:
Distance:
Apparent diameter:
Colongitude:
Phase:
Lunation:
Illumination:
Sub-solar latitude:
Libration in Latitude:
Libration in Longitude:
Position angle:
Azimuth
Altitude
Rise:
Transit:
Set:
Rise azimuth:
Transit Altitude:
Set azimuth:
3.. DETAILED REPORT
no wwv
iris/contrast problem
low light/obstructions?
good images
sharp limb
imagers good/ perfect for backdrop
and our work
39:00 images degraded
improved again
great rays
Theophils, Cyrillus
and catherina
Deter @ 52:00
1h31m45s eom
time fix
4. EQUIPMENT
RECORDERS
VHS1 on LIMA 2 (Quad)
VHS2 on LIMA 2 (VMA/SkyCam IR [B Cam] on Quad Cam 3 position)
VHS3 on LIMA 2 (CabCam, color, Quad Camera 2 position)
DVR1 on LIMA 2 (Q Sel)
DVR2 on LIMA 1 [default] (SSI Camera, Quad Cam 4 position)
QUAD CAMERA POSITIONS:
All camera outputs to Quad SAMSUNG SCQ-041P
Camera 1 mini finders (SC-NVA5’s), A (wide angle) & B
(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/T1392 E-M Datalogger/SkyCam IR (LPI /
C8 (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
Compaq Presario sr1218nx computer (1)
Digital to Analog Converter 1; TEP-100 Elite Pro II
VIRTUAL MOON ATLAS graphics left
EM DATALOGGER T1392 right set for
( X ) MilliGauss ( ) MicroTesla
( ) KII on rod for CabCam pickup
Aperture video recorder VHS2
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 ‘
SKYCAMS
Camera 3, CX480
Camera 4,
CONFIG:
(X) SSI in scope
back
( ) Diagonal and ( ) binoc viewer. Extended hand
control DOB Driver II