DELETED, (Qa%cra) Projort 5,1 = In-Plicht Participation of P-47 Aircraft Tt Robert C, Lawrann is to mcacure the blast, cust and nuclear dctonation on an in-flight B-47 aircraft, ts thermal effects of 0 The cbjective cf this preject cr OPITOTIVE With the recorded data, the criteria and method used in the P-47 Weapon Delivery Nandikcok may be verifici cr corrected. In additicn, the pro- jeet will provide pre basic research data for the design criteria of future USAF atreraft, INSTRIMTITATION oO Taree hundred ani thre data channels were avatlatle on this shot to reeord beniing, shear and torcfon in the wing end horpizontsl] stcbilizer, vhermal inprie te the aireraft, thermally induced strain, temperature meae surcments and overpressure. Fricr ic chst participaticn 94.7% of these Channels were cpcrating satisfactorily. Since the last participation mé angular acctelcromcter and one elevator camera have been added. ATPURATS POSTTION TN SrAcse The B-47 was flying at an absolute altituie of 24,009 feet, a speed of Mach ©,79, and on a headirg of 270° at both T and shock arrival. At T,) the horizontal range beyond ground zero was 11,000 fect, and at shock arrival it was approximately 31,69 feet, Sherrat A WEE: o-pcraturc rise was measured in the 0.020 in. 24ST aluminum right aileron test panel painted with 1.0 absorptivity black paint. A MRE: enpereture rise was recorded on the 0,025 in. aluminum right yh.ph COPIED/Dog LANL RC nl