LUNASCAN  MISSION  REPORT:   Session # 20150427 – 02 - 84  




========================================================================================================

1. QUALCOM SYNOPSIS:

Mission #2 for 2015 was successful and AOT was at 19:38:11 Quad Time/7:38:11 local. The duration of the mission was 1 hour 25 minutes 10 seconds, mission terminated at 21:02 Q. WWV was good on all recordings once the problem was realized. The aluminum shield of the trailer with the Sennheiser receiver inside was the culprit, so opening the door wider helped. Reception still varied however. At 20:10:43 there was a good WWV fix with a data stream and another fix at 20:12:04 = 00:40:22 EL =0108m00s CUT time fix.

Cam 4/SSI camera had good images. Elapsed 00:06:19 Good Tycho, etc. 00:11:51 Mons Piton, etc, Apennines. At  00:13:18 eastern crater rim on Copernicus  illuminated by rising sun. Crater interior not illuminated but complete rim was lit during the mission.

EOM at 21:02:00 Q



2. EPHEMERIS:      DE421


Observatory:    +3734' +8732' Tz: -4h00m
Date:   2015-04-27 19:30:00
Date (TT):      2015-04-27 23:31:09
(J2000) Right Ascension:        10h01m06.14s
(J2000) Declination:    +0809'55.3"
(Date) Right Ascension: 10h01m55.20s
(Date) Declination:     +0805'19.5"
Distance:       399370Km
Apparent diameter:      29.92'
Colongitude:    19.3
Phase:  68.2
Lunation:       9.19 days
Illumination:   68.6%
Sub-solar latitude:     -0.7
Libration in Latitude:  +0442'
Libration in Longitude: +0259'
Position angle: 21.5
Azimuth +12952'
Altitude        +5002'
Rise:   14h51m
Transit:        21h32m
Set:      3h33m
Rise azimuth:   +7824'
Transit Altitude:       +61
Set azimuth:    +28330'

 




===========================================================================================

3. DETAILED ANALYSIS:
Mission 84; 20150427

19:31:40 Q
19:36:50 AC trans / no WWV fix
19:38:11 AOT
Note incorrect VMA?
20:10:43 Good WWV w/message
20:12:04 = 00:40:22 EL =0108m00s CUT time fix
21:02:00 EOM
Mission time = 1h25m10s duration

CabCam good
Slight audo warble. Ck VCR rec on next mission.

SSI
Elapsed
00:06:19 Good Tycho, etc.
00:11:51 Mons Piton, etc, Appenines
00:13:18 E. edge of Copernicus, growing during mission.
00:29:18 AC trans
00:38:35 WWV on
00:40:10 = 01h8m CUT
01:10:03 DVD locked on SSI
Attempted reacq on Q-Sel, similar problem
01:24:08 = 01h52m00s CUT time fix

EOM at 21:02:00 Q



============================================================================================


4. EQUIPMENT MODE LEVEL

 

RECORDERS
VHS1 on LIMA 2 (Quad)
VHS2 on LIMA 2 (VMA/LPI Cam on Quad Cam 3 position)
VHS3 on LIMA 2 (CabCam, color, Quad Camera 2 position)

VHS 4 on LIMA 2 Skycam (B Cam on Cam position toggle)


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   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 RAM
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

HP dc5000MT Pentium 4
2.8 GHz, 512 MB RAM, 40 GB hard drive
Microsoft Windows XP Professional
Digital to Analog Converter 1; TEP-100 Elite Pro II

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
CMOS sensor by Hynix ~310kPix, (Bayer matrix), Complementary Metal Oxide Semiconductor Semiconductor Inc.
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 RAM,
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