My WebLink
|
Help
|
About
|
Sign Out
Home
Browse
Search
WMOD00317
CWCB
>
Weather Modification
>
DayForward
>
WMOD00317
Metadata
Thumbnails
Annotations
Entry Properties
Last modified
7/28/2009 2:35:48 PM
Creation date
3/11/2008 2:44:23 PM
Metadata
Fields
Template:
Weather Modification
Contract/Permit #
14-06-D-6999
Project Name
CAWRP
Title
Cascades Atmosphere Water Resources Program - Volume I
Prepared For
US Department of the Interior Bureau of Reclaimation
Date
7/1/1970
Weather Modification - Doc Type
Report
Jump to thumbnail
< previous set
next set >
There are no annotations on this page.
Document management portal powered by Laserfiche WebLink 9 © 1998-2015
Laserfiche.
All rights reserved.
/
266
PDF
Print
Pages to print
Enter page numbers and/or page ranges separated by commas. For example, 1,3,5-12.
After downloading, print the document using a PDF reader (e.g. Adobe Reader).
Show annotations
View images
View plain text
<br />In extensive flying under severe conditions in cyclonic storms over the <br /> <br /> <br />Cascade Mountains during the winter of 1970-71, the B-23 aircraft proved to <br /> <br /> <br />be a reliable and excellent aircraft for cloud physics research. <br /> <br /> <br />1.2 Conversion of the B-23 Aircraft for Cloud Physics Researcb <br /> <br /> <br />The B-23 arrived in Seattle on September 2,1970. Work began immediately <br /> <br /> <br />on modifying the aircraft and instrumenting it for research purposes. The <br /> <br />first stage of this work was finished by December 1, 1970, and from that time <br /> <br /> <br />on the aircraft was available for research purposes. ~owever, improvements <br /> <br />and additions continued to be made throughout 1971. The description given <br /> <br /> <br />below is of the aircraft research facility as it existed at the end of 1971. <br /> <br /> <br />To provide a large area for research equipment within the 'aircraft and <br /> <br /> <br />t'edllce excess weight to a minimum, all excess items (e. g . galley , extra seats, <br /> <br /> <br />tables, carpets, etc.) were removed. Two continuous, heavy duty seat tracks <br /> <br /> <br />were then installed on one side of the aircraft, in both the front and rear <br /> <br /> <br />cabins, on which equipment could be mounted and secured. Provision for sway <br /> <br /> <br />bracing was provided by a single track attached to the wall just below the <br /> <br /> <br />windows. With this system equipment could be placed at any position along <br /> <br /> <br />the tracks and removed without tools. <br /> <br /> <br />The wall panelling beneath the windows was removed and replaced by a <br /> <br /> <br />specially constructed panel which has two exterior trays with hinged lids, <br /> <br /> <br />one beneath the other, which run the length of. the cabin. These trays, which <br /> <br /> <br />have outlet boxes every few feet, served both as conduit and electrical <br /> <br /> <br />shields for the electrical wiring to the research instruments. One tray is <br /> <br /> <br />used for power lines and the other for signal lines. The power lines provide <br /> <br />110V - 60Hz, 110V - 400Hz and 28Vdc to each outlet box. The outlets are not <br /> <br />I- <br />I- <br />I- <br />I- <br />I <br />I <br />I <br />I- <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />
The URL can be used to link to this page
Your browser does not support the video tag.