DEAR AL:

Document Type: 
Collection: 
Document Number (FOIA) /ESDN (CREST): 
CIA-RDP67B00511R000100110028-9
Release Decision: 
RIFPUB
Original Classification: 
K
Document Page Count: 
5
Document Creation Date: 
December 14, 2016
Document Release Date: 
November 20, 2002
Sequence Number: 
28
Case Number: 
Publication Date: 
October 3, 1963
Content Type: 
LETTER
File: 
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PDF icon CIA-RDP67B00511R000100110028-9.pdf219.59 KB
Body: 
Approved ? Release 2003/01/24: CIA-RDP67B0.1 R0001 0b110028-9 OSA-5255-63 3 October 1963 As a result of the 26 September meeting on personal and life support equipment, several problem areas were clarified and responsibilities of contractors defined. Following is a recap of the conclusions of the meeting as they effect the Firewel Co. Problem: Oxygen consumption vs. ships supply. Discussion and action: It was agreed that 25 liters per minute be accepted as a base line from which to compute duration vs. supply.,, Cockpit pressurization at 26,000 ft. will remain the same. A failure of one system at mission mid-point is possible and sufficient oxygen must be available for safe return on the remaining system. By the end of November of this year the larger oxygen bottles, 3.100 cu. in. vs. the present 875 cu. in., will be installed. These bottles will be charged to 2800 PSI vs. the present 2000 PSI. Problem: Readability of ships oxygen pressure gauge. Action: A top priority item for Firewel Co. to provide a gauge that can be read quickly and accurately. LAC may have to relocate the gauge to eliminate paralax error. Problem: Oxygen Equalizer Valve Discussion: This device is required to insure that both ships oxygen systems bleed down together. To date, Firewel Co. has not been able to produce an acceptable valve. Action: Firewel will continue working on the problem and LAC will try their own approach. Problem: Vent flow back pressure In full pressure suit. Action: Firewel will investigate change of flow at different detent positions on the flow controller. They will also investigate the bigger problem of why so much volume is required for adequate cooling. This problem has not been encountered in chamber runs. Problem: Manual press to test. Action: Item has met with pilot approval however, a more coarse control is desired - Firewel will provide. Problem: Vent hose disconnecting. Action: Firewel procuring hoses that . are. tiro inches longer. Approved For Release 2003/01/24: CIA-RDP67BOO511 R000100110028-9 Approved* Release 2003/01/24: CIA-RDP67B11R000100110028-9 Page 2 Problem: Floating position of pilot in full pressure suit. Discussion and Action: In a pool demonstration the subject was able to float in face down position. However, the parachute harness did not include the emergency oxygen pan or the automatic timer pan. Firevel to provide harness with these features plus a survival kit for future tests. Previous jump tests indicated proper floating -position. Problem: Release of emergency oxygen hose connection at suit- controller. Action: Firewel recently modified this connection which is being. evaluated by the pilots. It is hoped the above recap will serve as a guideline for your future effort. Regards, $arry Ca Approved For Release 2003/01/24: CIA-RDP67BOO51 1 R0001 00110028-9 Approved0 Release 2003/01/24: CIA-RDP67BOO I R0001 00110028-9 OBA-5254-63 4 October 1953 As a result of the 26 Bapteaber meeting on personal and life support equipment, actions to be taken by several contractors were defined. The problems, discussion, end action as related to LAC are as follows: Problem; amen consumption vs. d2ips supply. ft~ Discussion and action- It waa agreed that 25 liters per minute be accepted as a base line from ithich to compute duration vs. supply. Cockpit pressurization at 26,000 ft. will, remain the same. A failure of one system at mission mid-poi, is possible and sufficient oxygen must be available for safe return on the remaining system. By the end of November of this yew the larger oxygen bottles, 1100 Cu. in. vs. the present 875 cu. in.,, will be instaalled. These bottles will be charged to FBI vs. the present 2000 PSI. When the larger bottles, charged to the higher pressure, are installed, a mission of eight ham and fifteen minutes is possible with failure of one systemm at mission mid-point. This assumes a consumption rate of 25 liters peer minute. The possibility of charging the bottles to 3000 PBX will be pursued by Firewel. Co. Problem: Readability of ships oxygen pressure gauge. Action: A top priority item for Firew el Co. to provide a gauge that can be read quickly and accurately. LAG may have to relocate the gauge to eliminate parelax error. Problem; oxygen Equalizer Valve Discussion- This device is required to insure that both ships oxygen systems bleed down together. Tb data, Fireswel Co. has not been able to produce an acceptable valve. Action: Firewel will continue working on the problem and LAO will try their own approach. Approved For Release 2003/01/24: CIA-RDP67B00511 R000100110028-9 Approved For lease 2003/01/24: CIA-RDP67B0051 000100110028-9 X11-525 13 Palms I Problem: Neck Beal vs. teem Seal in full pressure suit helmet. Discussion: Two LAC pig and two of our pilots have suits with the neck seal. "lights vin,_0ontinue with these garments to gather additional information reg fiag oxygen consumption and comfort. Ejection Seat D Ring. Discussion: A new D ring configuration was mocked up and checked with subject pressurized. Sbe subject was able to reach the D ring under pressure, however, the back up system D ring vas barely reachable. Action: LAC will it ro back up "ton D ring. Proms: Location of visor heat control. Action: Although this contrat has been moved fbrward four inches, the subject could not reach it t o the suit was pressurized. LAC Will attempt to make the control more accessible. Problan> Leg stretch Action: .AC will provide new rudder configuration that will allow full leg stretch then desired. Problem: Lap belt failure. Discussion: A lap belt failure in an ejection seat test at El Centro prevented dummy and seat separation. LAC investigated the problem and found that the force required to sheer the pin varied from 450 PSI to 850 PSI. This was caused by pin heat treat thich ranged from 55,E PSI UTS to 110,000 PSI UT IL Actions LAC is replacing the presently installed shear pin with one which has a controlled heat treat of 55,000 PSI UN to 66,000 PSI UTS maximum. Problem: Oxygen pressure wing light. Discussion: Pilots desire an oxygen pressure warning light to indicate low breathing pressure or possibly both low and high oxygen pressure. Action: LAC will investigate. Approved For Release 2003/01/24: CIA-RDP67B00511R000100110028-9 Approved For .ease 2003/01/24: CIA-RDP67B0051000100110028-9 OBA-525"3 Page 3 A meetinG of headquarters representatives wM be held early next week regarding the present parachute and the integrated harness. I will keel you informed on the decisions reached. Regards: Harry C. Approved For Release 2003/01/24: CIA-RDP67BOO511 R000100110028-9