PEIPING MISSILE DEVELOPMENT AND PRODUCTION CENTER CHANG-HSIN-TIEN, CHINA OCTOBER 1965

Document Type: 
Document Number (FOIA) /ESDN (CREST): 
CIA-RDP78T04759A002200010086-9
Release Decision: 
RIPPUB
Original Classification: 
T
Document Page Count: 
7
Document Creation Date: 
December 28, 2016
Document Release Date: 
May 17, 2011
Sequence Number: 
86
Case Number: 
Publication Date: 
December 1, 1965
Content Type: 
REPORT
File: 
AttachmentSize
PDF icon CIA-RDP78T04759A002200010086-9.pdf1.1 MB
Body: 
Sanitized Copy Approved for Release 2011/05/17: CIA-RDP78TO4759AO02200010086-9 PHOTOGRAPHIC INTERPRETATI REPO PEIPING MISSILE DEVELOPMENT AND PRODUCTION CENTER CHANG-HSIN-TIEN, CHINA OCTOBER 1965 DECEMBER 1965 COPY 4 PAGES GROUP 1 FXCLUDFfl PRO. AUTOMATIC DOWN~3RADIP.G AND DECLASSIFIC::-110N 11,4 TOP SECRET Sanitized Copy Approved for Release 2011/05/17: CIA-RDP78TO4759AO02200010086-9 Sanitized Copy Approved for Release 2011/05/17: CIA-RDP78TO4759AO02200010086-9 Sanitized Copy Approved for Release 2011/05/17: CIA-RDP78TO4759AO02200010086-9 Sanitized Copy Approved for Release 2011/05/17: CIA-RDP78TO4759AO02 PEIPING MISSILE DEVELOPMENT AND PRODUCTION CENTER CHANG-HSIN-TIEN, CHINA OCTOBER 1965 The Peiping Missile Development and Pro- duction Center Chang-hsin-tien (PMDPC,C is 3 nautical miles (nm) west of Chang-hsin-tien and 13 nm southwest of Pei- ping, China, at 39-49-30N 116-08-OOE (Fig- ure 1). The major components of the PMDPC are the Rocket Engine Test Facility, the Main Administration Area, the Industrial/Research and Development (R & D) Area, the thermal powerplant, and 2 housing areas. October 1965KH-7 KEYHOLE photography of the cen- ter is excellent, and several significant fea- tures have been identified in the Rocket En- gine Test Facility and in the Industrial/R & D Area. An analysis of earlier photography 200010086-9 of the installation indicated that some of these features existed in September 1961 and Novem- ber 1964. The Rocket Engine Test Facility occupies the northern portion of the PMDPC and consists of 3 vertical test stands, a horizontal test site, 2 assembly/checkout buildings, a components test area, and several support buildings (Fig- ure 2). Construction activity north of the test stands has been identified as a possible pro- pellant production area under construction. The area contains 2 vented production buildings, 2 storage tanks, and a small structure, all of which are interconnected by ditches for under- ground pipelines. Two support buildings, sev- eral small structures, and a possible storage tank are situated nearby. In the Components Test Area cast of the vertical test stands, principal facilities include 2 components test buildings and a possible components test build- ing which was identified in October 1965. The westernmost test building, the largest of the 3, apparently contains a single test position; the middle test building contains 2 test positions; and the easternmost possible test building, the smallest of the 3, appears to contain 2 test positions. The roofs over all test positions appear to have been constructed so that an accidental explosion would be forced upward. The area also contains a control building and several support buildings. At the vertical test stands contaminant stains are visible in the sumps used for catching runoff from the water cascade cooling systems. Three rail cars and a probable switch engine were observed near the middle test stand. TOP SECRET RUFF 25X1 25X1 Sanitized Copy Approved for Release 2011/05/17: CIA-RDP78TO4759AO02200010086-9 Sanitized Copy Approved for Release 2011/05/17: CIA-RDP78T04759A002200010086-9 TOP SECRET RUFF -2- TOP SECRET RUFF Sanitized Copy Approved for Release 2011/05/17: CIA-RDP78T04759A002200010086-9 25X1 25X1 Sanitized Copy Approved for Release 2011/05/17: CIA-RDP78TO4759AO02200010086-9 iur JtuKtI Kurr NPIC K-6771 (12/66) FIGURE 3. WIND TUNNEL IN THE INDUSTRIAL/R 8 D AREA, OCTOBER 1965. The Industrial/R & D Area is south of the Rocket Engine Test Facility and consists of research and development, industrial, admin- istration, and housing facilities. The area is rail served, and a surfaced road extends directly to the Rocket Engine Test Facility. In the separately secured southwest section of the area an irregularly shaped structure has been identified as a continuous-flow wind tunnel (Figures 2 and 3). It was not present in March 1964 but was observed in November 1964; at the present time it is nearing com- pletion. The tunnel measures 240 feet long overall and has a model preparation, mounting, and recording section measuring 135 by 60 by approximately 50 feet high. The outside of the flow chamber is square rather than round. A row of several curved objects re- sembling segments of circular tunnel sections NPIC K-6772 (12/65) FIGURE 4. CYLINDRICAL OBJECT IN THE INDUSTRIAL/R 8 D AREA, OCTOBER 1965. or a large conduit are situated northeast of the wind tunnel. A large group of horizontal pressure-type tanks, a bank of cooling towers, and 3 large buildings are situated near the wind tunnel and resemble facilities for gas dynamics, supersonic wind tunnels. The pres- sure-type tanks and the 3 buildings were pres- ent in September 1961. The open storage yard in the northeast section of the Industrial/R & D Area contains a light-toned cylindrical object situated near a ponent, such as a sonic test chamber or a vacuum aspirator. 25X1 25X1 TOP SECRET RUFF Sanitized Copy Approved for Release 2011/05/17: CIA-RDP78TO4759AO02200010086-9 Sanitized Copy Approved for Release 2011/05/17: CIA-RDP78TO4759AO02200010086-9 w r JtLKt I KUtt SAC. US Air Target Chart, Series 200, Shoot 0381-1AL, 2d ed, Jul 60, scale 1:200,000 (SECRET) TOP SECRET RUFF Sanitized Copy Approved for Release 2011/05/17: CIA-RDP78TO4759AO02200010086-9 Sanitized Copy Approved for Release 2011/05/17: CIA-RDP78T04759A002200010086-9 iur JCut(G 1 TOP SECRET Sanitized Copy Approved for Release 2011/05/17: CIA-RDP78T04759A002200010086-9