PRELIMINARY EVALUATION OF THE OXCART CONTRAIL PROBLEM

Document Type: 
Collection: 
Document Number (FOIA) /ESDN (CREST): 
CIA-RDP81B00879R001000090162-7
Release Decision: 
RIPPUB
Original Classification: 
T
Document Page Count: 
2
Document Creation Date: 
December 15, 2016
Document Release Date: 
October 25, 2002
Sequence Number: 
162
Case Number: 
Publication Date: 
August 10, 1962
Content Type: 
MF
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PDF icon CIA-RDP81B00879R001000090162-7.pdf116.24 KB
Body: 
Approved For elease 2002/1 OXC-3818-62 10 August 1962 Copy_ Of C DDAU1i W8! D?,Tk: MEMORANDUM FOR: Chief, Development Division, O.SA/DD/R SUBJECT Preliminary Evaluation of the OXCART Contrail Problem REFERENCE OXC-3538-62, dated 23 May 1962, Memo for Chief, Development Branch, DPD/DD/P 1. The previous paper, referenced above, is a general discussion of the subject of possible contrail formation at altitudes between 80,000 and 100,000 feet. This paper presents the results of further investigation, with most of the information summarized in graphic form. At our request, the Air Weather Service Climatic Center compiled the necessary temperature data in statistical form. This was no small task, since representative data could be obtained only by extracting thousands of interpolated readings from individual analyzed weather charts. 2. Figures 1, 2, and 3 are cumulative frequency graphs of the tem- perature distribution near the 100,000 foot level, between latitudes of 500 to 800 North. Individual charts are presented for the summer period, the winter cold period and the winter warm period. Separate charts are presented for the two types of winter temperature regimes because the temperature distribution during that season is markedly bimodal. The colder temperatures are believed to prevail about two-thirds of the time, while the warmer temperature regimes prevail during the remaining third. The changes from warm to cold, and vice versa, take place rapidly. Thus, the arithmetic mean of the observed temperatures occurs only a small per- cent of the time. 3. Figure 4 is a graph of the probability of contrail formation versus altitude, temperature and relative humidity. The various contrail zones determined from this graph are indicated on figures 2 and 3. None of the temperatures plotted on figure 1, fall within the contrail range. 4. Figure 5 is a graph of the probability of contrail formation versus altitude and latitude along certain longitudes. The longitudes were selected on the basis of proximity to possible OXCART mission tracks and availability of high altitude temperature data. The chart is applicable to the winter period, October thru March, only. During the remainder of the year, temperatures at the altitudes and latitudes con- sidered are not cold enough for contrails to form. Both figures 4 and 5 are based on data and computations pertaining to aircraft with turbojet engines, using JP-4 fuel. ^` LPp "_ R i' T 00090162-7 czctu. fr a itam3tic Approved FoKOIease 2002E 114 :)-O'81 B0087Q001000090162-7 5. The most definitive statement that can be made at this time is that, during the winter months, there is at least a 30% probability that the A-12 will produce contrails over a significant portion of a polar mission route. A critical factor in the detection of these contrails, by an observer on the ground, would be the degree of illu- mination at the altitude where the contrails were produced. 6. The weakest link in any evaluation of this problem is the lack of specific flight data from the A-12. Before the critical contrail formation temperatures applicable to the A-12 can be determined, numerous positive and negative contrail reports, coupled with specific altitude and temperature data, must be obtained over the full operating range of this aircraft. These observations should be made with the A-12 equipped with the engines and fuel it will use during operational missions. Major USAF Chief, Weather Staff, OSA/DD/R Distribution: Copy 1 - AD/OSA/DDR 2 - DD/OSA/DDR 3 - OD/OSA/DDR 4 - Staff Weather Office 5 - Weather Staff, OSA/D 6 - RI/QSA/DDR This do^cru t acts i Eftr?iation referring to Project 25X1A SECRET Approved For Release 2002/11/14(-: CLA-RDP81B00879R001000090162-7 1`_ cRooi- ~ l Excluded frci a!ltamatic dnwnurs:in ani E