The information on this second history page was provided by Capt Dan A. Shaltanis, HQ AFWA/XOOR, the Air Force Weather Agency (the old Global Weather Central). It's a very informative and interesting read on the early program history and chronology. At the bottom of this page an additional link to a more personal history page is provided where members may contribute their own personal recollections and unique experiences.
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Defense Meteorological Satellite Program History
Program Inception
In 1960 it became clear to Dr J. V. Charyk, Undersecretary of the Air Force, that the operation of certain highly classified military programs could be significantly enhanced if cloud cover over the Eurasian continent were known accurately on a daily basis. Inquiry as to the capability of the National Meteorological Satellite Program (or National Operational Meteorological Satellite (NOMS), under development by the NASA and the US Weather Bureau, to meet this need was made. After thorough analysis it was determined that the critical period when Eurasian coverage was required would occur in Summer, 1962, and the National System could not meet the needs; therefore, a plan for a one time, single purpose, minimum cost program was developed, approved and funded.
Program Constraints
By direction of DOD and the Undersecretary of the Air Force, the program, originally named Program 35, then changed to Program 417 or the Defense Satellite Applications Program (DSAP), was approved on 21 August 1961 subject to the following constraints:
a. Strict security provisions would prevail. Certain special management aspects and the mission itself would be considered especially sensitive to protect other highly classified programs interfacing with P-35 and to prevent embarrassing the United States in international relationships concerning the acquisition and distribution of meteorological data. Knowledge of the program would be held to the absolute minimum number of persons required to conduct the program.
b. A hard funds ceiling and program schedule (10 million dollars and 9 months to first launch) was imposed with direction to terminate the program without further instructions if either was to be exceeded.
c. All equipment would be purchased on fixed price contracts. Maximum use would be made of existing design and techniques and development work would be held to a minimum.
The program director would report directly to the Undersecretary of the Air Force, in person, at monthly intervals. Other program reporting, except essential planning, fiscal and historical records, was to be waived.
Program Office
A program office was originated within the Space Systems Division, Air Force Systems Command (AFSC), in Los Angeles, CA. The office and its method of operating were significantly different form other programs in SSD in the following ways:
a. A total of only five officers and two secretaries were authorized. (The average SSD program office at the initial stage of a program consists of 36 Persons.) This small office was justified by the expected short duration of the program, the prohibition on development work, and the elimination of normal program reporting requirements.
b. It was decided not to use Aerospace Corporation or other "System Engineering and Technical Direction" contractor. The requirements for fixed schedule, fixed funds ceilings and fixed price contracting were completely incompatible with the SE/TD type of operation normal to SSD programs, and Aerospace Corporation was unwilling to accept a different role.
c. The program office was deleted from all SSD organizational charts, etc. The unusual reporting procedures and requirement for special security precautions made it advisable to avoid calling attention to the program office.
d. Consistent with the above, it was decided to perform as much as possible of the systems engineering, program documentation, operations performance analysis, etc. entirely within the program office rather than to use contractor or SSD staff support offices. Exceptions were procurement of boosters and participation of computer programs necessary for on-orbit support.
Original Responsibilities
Under the overall authority of the program office the following specific responsibilities were assigned:
a. Booster Procurement (Scout vehicle) was handled by the SSD Blue Scout program office. Direct fixed price contracts were negotiated with Ling-Temco-Vought and Aerojet for booster hardware and first stage motors respectively. A firm price agreement was arranged through the Army's Redstone Arsenal for the second stage motors which were supplied by Thiokol to the Army on a captive contract. Third and fourth stage motors were to be supplied by Allegany Ballistic Laboratories through the NASA captive contract on a guaranteed price basis.
b. Launch support was provided by the 6595th Aerospace Test Wing with support from NASA and Ling-Temco-Vought. Most of the Scout vehicle launch crew were Air Force personnel who had previously launched Blue Scouts from AMR.
c. Satellites were bought from RCA Astro-Electronics Division on a fixed price contract by the program office.
d. On orbit support was provided by the 6594th Aerospace Test Wing with supporting contracts administered by the SSD Satellite Control Office. On-orbit control was exercised by the Satellite Test Center in Sunnyvale, CA through the Vandenberg AFB, CA and New Boston, New Hampshire, tracking and readout stations and was operated by RCA personnel on contract to the program office.
Orbital Operations
From August 1962 until July 1963 on-orbit operations were directed from the Satellite Test Center (AFSC) at Sunnyvale, CA. A mixed team of AF and RCA personnel provided engineering analysis backup to the 6595th ATW controllers. The tracking and readout stations at Vandenberg AFB and New Boston, New Hampshire, had video reconstruction and command generating equipment peculiar to this program manned by RCA technicians. Data were recorded at the readout stations and then transmitted to the Air Force Global Weather Center (GWC) at Offutt AFB, NE via land line where the pictures were reconstructed for analysis. Transmission was made at quarter speed to reduce bandwidth requirements and line costs. Tracking support was furnished from the outset by Spacetrack which supplied vector parameters to the STC where and expanded ephemeris was produced.
After 1 Jul 63, operations were shifted to special ground stations located at surplus Nike missile sites near Loring AFB, Maine, and Fairchild AFB, WA. These stations consist of advanced design 40-ft diameter antennas operating in a pneumatic radome, and three mobile vans; one each for communications, video reconstruction and command, and antenna controls and receivers. These stations are controlled from a minimum communications and control center at Offutt AFB. The 4000th Support Group (Strategic Air Command (SAC)) mans the stations and center completely including a computer support facility (shared with other SAC operations) and a systems Analysis Division which provides full technical backup to the operators and controllers. Further technical backup for abnormality analysis, etc., is provided by the 417 SPO and an analysis group in RCA/AED. Overall technical and configuration control is exercised by the 417 Program Office through a System Concept and Procedures (SCAP) document which contains detailed procedures for every man in the system for both normal and abnormal operations. The SCAP is continuously updated by the 417 SPO with 4000 Spt Gp assistance. Completely detailed ground equipment drawings are maintained by AFLC at SMAMA and all logistics support is furnished by a Systems Support Manager at SMAMA. Training requirements for all military personnel have been met by the Air Training Command.
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Early Program Chronology
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19 Jul 61 |
Conditional approval to proceed with program planning |
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29 Jul 61 |
Satellite contract written and negotiated. Authority to proceed withheld pending successful booster negotiations. |
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21 Aug 61 |
Booster contracts completed. Approval to start work given to all contractors. |
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26 Oct 61 |
Unsatisfactory performance and schedule of NASA sponsored Scout fourth stage motor (ABL-258) noted at NASA-DOD coordination meeting |
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3 Nov 61 |
National range documentation completed entirely by program office |
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8 Nov 61 |
ABL-258 motor failed seventh time out of seven tests |
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16 Nov 61 |
Directed development of substitute motor (MG-18) for fourth stage of Scout by Lockheed Propulsion Corporation through 6594th Test Group, Edwards AFB, CA |
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25 Feb 62 |
Spacecraft prototype destroyed in vibration tests. Preliminary actions taken to terminate program. "Cure" notice sent contractor per ASPIR |
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13 Mar 62 |
Spacecraft structure redesign, refabrication and retest complete. Program back on schedule |
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2 Apr 62 |
MG-18 motor successfully fired in vacuum at Arnold Engineering Development Center |
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13 May 62 |
First 417 count-down scrubbed due to Scout hydraulic system failure |
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23 May 62 |
First 417 launch unsuccessful when Scout second stage exploded |
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23 Aug 62 |
Second launch attempt successful. Satellite operating normally in orbit |
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24 Oct 62 |
Authority to rebuild program peculiar ground stations received. |
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27 Oct 62 |
Direct readout station "Leda", in full operation at Eglin AFB |
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15 Nov 62 |
Third 417 booster and satellite placed in R-5 days stand-by status for indefinite period |
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26 Nov 62 |
Contractor started work on second set of four satellites |
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10 Dec 62 |
Discontinued operation of station "Leda" at Eglin AFB |
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17 Dec 62 |
total satellite capacity used for 24-hour period to give complete daylight map of Antarctica |
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19 Feb 63 |
Third 417 launch resulted in elliptical orbit due to poor third stage performance. Satellite operating normally |
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8 Mar 63 |
Fixed price contract for new ground stations issued to Radiation Incorporated following full competitive bid-evaluation board procedures |
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26 Apr 63 |
Fourth launch attempt failed with Scout third stage explosion |
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20 May 63 |
Because of continuing slip of the National Meteorological Satellite program, direction was received to build six additional satellites and boosters (total of 14) |
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14 Jun 63 |
Study of Scout reliability concludes primary cause of poor performance is poor program management by NASA. Extensive improvements recommended. |
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24 Jun 63 |
Patent disclosure filed by 417 Program Office on "DC motor" method of satellite spin control |
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1 Jul 63 |
On-orbit operations shifted to program peculiar ground stations and control center. Manning is 1200 per cent military |
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14 Aug 63 |
Logistics and maintenance support responsibility for 417 ground stations assumed by Air Force Logistics Command (AFLC) (SMAMA) |
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27 Sep 63 |
Fifth launch attempt failed with loss of Scout attitude control after third stage burn |
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23 Oct 63 |
Direction received to cancel all Scout activities; recoup all recoverable Scout funds from NASA; proceed with dual spacecraft launch form Thor-Agena at earliest possible date |
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31 Oct 63 |
Modified last three of current buy of six satellites to include DC spin control and other improvements |
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26 Nov 63 |
Directed to prepare plan using Thor/MG-18 booster configuration. Later nicknamed "Burner I." |
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23 Dec 63 |
Burner I plan approved. Implementation to be expedited |
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19 Jan 64 |
Satellites six and seven successfully launched from Thor-Agena. Both operating perfectly |
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7 Feb 64 |
Approval granted to kill satellite launch 19 Feb 63 since spin is too low to maintain altitude |
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17 Mar 64 |
Development of advanced IR system approved. Second Thor-Agena launch approved. Directed to proceed with System Definition Phase for Burner II |
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18 Jun 64 |
Second Thor-Agena launch placed spacecraft eight and nine in optimum orbit. Orbit velocity adjust included in F9 |
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19 Jun 64 |
Per USWB request, procedures established to provide 417 data on tropical disturbances because Tiros data are inadequate. Code name, "Loose Talk" |
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28 Jul 64 |
Satellite F6 launched 19 Jan 64 killed because spin rate too low to operate |
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2 Sep 64 |
Fully funded fixed price contracts issued to Boeing Company and Ling-Temco-Vought for Phase I for Burner II |
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20 Nov 64 |
Directed to place tactical readout station near Saigon and to proceed to build special satellite (F15) |
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11 Jan 65 |
Directed to procure four more satellites with dual tactical/global capability (F16 through F19) |
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18 Jan 65 |
First Burner I launch carried satellite F10 to good orbit but satellite failed to separate form upper stage |
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28 Jan 65 |
Burner II Source Selection Board findings approved. Boeing will build stage |
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17 Mar 65 |
Satellite F7 launched 19 Jan 64 killed because spin rate too low to operate |
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18 Mar 65 |
Second Burner I launch placed F11 into good orbit. Satellite operating normally. Entire launch by military personnel |
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17 Apr 65 |
Tactical station at Tan Son Nhut Airfield completed and in operation |
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18 May 65 |
Third Burner I using advanced upper stage (UTC) motor FW-4S) placed special satellite F15 in good orbit. Satellite giving daily coverage to station in Viet Nam |
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A launch history follows |
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| Block 5D-3 | ||||
| Space Craft | Launched | International Desig. | Booster | Remarks |
| S-20 | Jul 08 | EELV | ||
| S-19 | Feb 07 | EELV | ||
| S-18 | Mar 05 | EELV | ||
| S-17 | Mar 03 | EELV | ||
| S-16 | Sep 00 | Titan | ||
| Block 5D-3 Hybrid (5D-2 Instruments, 5D-3 Bus | ||||
| Space Craft | Launched | Remarks | ||
| S-15 | L-16 Hold | Titan - Liftoff: 173804.393Z | ||
| Block 5D-2 | ||||
| Space Craft | Launched | International Desig. | Booster | Remarks |
| F14 | 2 Apr 97 | 1997-012A 24753 | Titan - Liftoff: 164703.740Z | |
| F13 | 24 Mar 95 | 1995-015A 23533 | Atlas E - Liftoff: 140500.580Z | |
| F12 | 29 Aug 94 | 1994-057A 23233 | Atlas E - Liftoff: 1738Z | |
| F11 | 28 Nov 91 | 1991-082A 21798 | Atlas E - Liftoff: 132300.225Z | OLS turned off 22 Aug 95 OLS turned on 5 May 98 |
| F10 | 1 Dec 90 | 1990-105A 20978 | Atlas E - Liftoff: 155735.789Z | 8 Feb 95 OLS turned off First RDS capable S/C |
| F 9 | 3 Feb 88 | 1988-006A 18822 | Atlas E - Liftoff: 055300.319Z | Non-Op 23 Feb 92 (1481 days) |
| F 8 | 16 Jun 87 | 1987-053A 18123 | Atlas E - Liftoff: 023359.868Z | Non-Op 13 Aug 91 (1513 days) 24 Nov 95-OLS Failed Used for SSMI until 15 Oct 97 |
| F 7 | 18 Nov 83 | 1983-113A 14506 | Atlas E - Liftoff: 063159.552Z | Non-Op 17 Oct 87 (1399 days) OLS bearing failure |
| F 6 | 21 Dec 82 | 1982-118A 13736 | Atlas E - Liftoff: 023447.697Z | Non-Op 24 Aug 87 (1708 days) OLS bearing failure First S/C with encryption |
| Block 5D-1 | ||||
| Space Craft | Launched | International Desig. NORAD Catalog # | Booster | Remarks |
| Flight 5 | 14 Jul 80 | Thor/Burner IIA | Launch Failure | |
| Flight 4 OPS 5390 | 6 Jun 79 | 1979-050A 11389 | Thor/Burner IIA | AMS-4 Non-Op 29 Aug 80 (430 days) Battery failure |
| Flight 3 OPS 6182 | 30 Apr 78 | 1978-042A 10820 | Thor/Burner IIA | AMS-3 Non-Op Dec 79 (580 days) OLS Failure |
| Flight 2 OPS 5644 | 5 Jun 77 | 1977-044A 10033 | Thor/Burner IIA | AMS-2 (solar array partially deployed) Non-Op 19 Mar 80 (880 days) spacecraft computer failure |
| Flight 1 OPS 5721 | 11 Sep 76 | 1976-091A 9415 | Thor/Burner IIA | AMS-1 (operational-36 mo) Battery Failure |
| Block 5C | ||||
| Space Craft | Launched | International Desig. NORAD Catalog # | Booster | Remarks |
| Veh # 11534 OPS 5140 | 19 Feb 76 | 1976-016A 8696 | Thor/Burner IIA | Launch Failure Re-entered 19 Feb 76 Booster ran out of fuel before achieving orbit |
| Veh # 10533 OPS 6226 | 24 May 75 | 1975-043A 7816 | Thor/Burner IIA | Non-Op 30 Nov 77 (922 days) Temperature problems |
| Veh # 9532 OPS 6983 | 8 Aug 74 | 1974-063A 7411 | Thor/Burner IIA | Non-Op 22 Nov 74 (114 days) Sensor mechanical failure |
| Veh # 8531 OPS 8579 | 16 Mar 74 | 1974-015A 7218 | Thor/Burner IIA | Non-Op 27 may 76 (802 days) Transmitter failure |
| Veh # 7529 OPS 8364 | 16 Aug 73 | 1973-054A 6787 | Thor/Burner IIA | Non-Op 24 Jan 77 (1257 days) Primary sensor degradation |
| Veh # 6530 OPS 7323 | 8 Nov 72 | 1972-089A 6276 | Thor/Burner IIA | Non-Op 21 Jun 73 (225 days) Sensor electrical failure |
| Block 5B | ||||
| Space Craft | Launched | International Desig. NORAD Catalog # | Booster | Remarks |
| Veh # 5528 OPS 5058 | 24 Mar 72 | 1972-018A 5903 | Thor/Burner IIA | Non-Op 23 Feb 74 (701 Days) Sensor Electrical Failure |
| Veh # 4527 OPS 4311 | 14 Oct 71 | 1971-087A 5557 | Thor/Burner IIA | Non-Op 27 Apr 72 (196 days) Heat from Burner IIA degraded performance and life |
| Block 5A | ||||
| Space Craft | Launched | International Desig. NORAD Catalog # | Booster | Remarks |
| Veh # 3526 OPS 5268 | 17 Feb 71 | 1971-012A 4953 | Thor/Burner II | Non-Op 3 Mar 73 (746 days) |
| Veh # 2525 OPS 0203 | 3 Sep 70 | 1970-070A 4512 | Thor/Burner II | Non-Op 15 Feb 71 (164 days) |
| Veh # 1524 OPS 0054 | 11 Feb 70 | 1970-012A 4331 | Thor/Burner II | Non-Op 30 Apr 70 (78 days) |
| Block 4 | ||||
| Space Craft | Launched | International Desig. NORAD Catalog # | Booster | Remarks |
| F-23 | On Display Wright-Patterson Museum | |||
| Veh # 7421 OPS 1127 | 23 Jul 69 | 1969-062A 4047 | Thor/Burner II | Non-Op 19 Mar 71 (604 days) |
| Veh # 6422 OPS 4078 | 22 Oct 68 | 1968-092A 3510 | Thor/Burner II | Non-Op 19 Sep 70 (697 days) |
| Veh # 5420 OPS 7869 | 23 May 68 | 1968-042A 3266 | Thor/Burner II | Non-Op 11 Sep 68 (112 days) |
| Veh # 4417 OPS 1264 | 11 Oct 67 | 1967-096A 2980 | Thor/Burner II | Non-Op 26 Mar 68 (167 days) |
| Veh # 3419 OPS 7202 | 23 Aug 67 | 1967-080A 2920 | Thor/Burner II | Non-Op 13 Mar 68 (204 days) |
| Veh # 2418 OPS 6073 | 8 Feb 67 | 1967-010A 2669 | Thor/Burner II | "Arrow Point" (low orbit) DSAP 2416 Non-Op 18 May 67 (99 days) |
| Veh # 1416 OPS 6026 FTV-3 | 16 Sep 66 | 1966-082A 2418 | Thor/Burner II | "Irish Duke" DSAP 1416 3 Nov 68 (780 days) |
| Block 2 | ||||
| Space Craft | Launched | International Desig. NORAD Catalog # | Booster | Remarks |
| Veh # 0513 OPS 0340 | 30 Mar 66 | 1966-026A 2125 | Thor/Burner I | "Resort Motel" Non-Op 30 Mar 68 (730 days) |
| Veh # 0714 | 6 Jan 66 | None | Thor/Burner I | Launch failure "Persian Lamb" Burner I failed to ignite |
| Veh # 0212 OPS 8068 | 9 Sep 65 | 1965-072A 1580 | Thor/Burner I | "Victoria Cross" DSAP 13 4A-F4 Non-Op 17 Aug 66 (341 days) |
| Block 1 | ||||
| Space Craft | Launched | International Desig. NORAD Catalog # | Booster | Remarks |
| OPS 8386 | 20 May 65 | 1965-038A 1377 | Thor/Burner I | "Royal Eagle" DSAP 12 |
| Flight Test Vehicle 0911 OPS 7353 | 18 Mar 65 | 1965-021A 1273 | Thor/Burner I | "Astral Body" DSAP 11 Jun 65 (3.0) Re-entered 31 Dec 89 |
| Flight Test Vehicle 0610 OPS 7040 | 19 Jan 65 | 1965-003A 973 | Thor/Burner I | "Astral Lamp" DSAP 10 Non-Op Jul 65 Re-entered 13 Jul 79 |
| OPS 4262 | 23 Sep 64 | 1964-058A 884 | Atlas D | "Buzzing Bee" Re-entered 28 Sep 64 |
| OPS 3497 | 14 Sep 64 | 1964-056A 882 | Atlas D | "Butterfly Net" Re-entered 6 Oct 64 |
| 29 Jul 64 | Atlas D | "Knock Wood" | ||
| Flight Test Vehicle 8099 OPS 4467B | 18 Jun 64 | 1964-031B 813 | Atlas D | "Iron Lung" Non-Op 15 Oct 65 |
| Flight Test Vehicle 6218 OPS 4467A | 18 Jun 64 | 1964-031A 812 | Atlas D | "Iron Lung" Two satellites #8, #9 Non-Op 16 Feb 66 Non-Op |
| Flight Test Vehicle 4187 OPS 3367A | 19 Jan 64 | 1964-002B 734 | Thor-Agena | Two satellites launched #6, #7 #7 Non-Op 17 Mar 65 #6 Non-Op 28 Jul 64 |
| Initial Launches | ||||
| Space Craft | Launched | International Desig. NORAD Catalog # | Booster | Program Name |
| 18 Dec 63 | Atlas D | "Lens Cover Q" | ||
| 17 Dec 63 | Blue Scout Jr. | -No Name- | ||
| 4 Nov 63 | Atlas D | "Hickory Hollow" | ||
| 417-5 | 27 Sep 63 | Scout | Launch Failure Third stage loss atitude control | |
| 12 Jun 63 | Atlas D | "Harpoon Gun" | ||
| 417-4 | 26 Apr 63 | Scout | Launch Failure Third stage exploded | |
| 417-3 | 19 Feb 63 | Scout | Elliptical Orbit due to poor third stage performance Non-Op 7 Feb 64 | |
| 417-2 | 23 Aug 62 | Scout | Operated Nominally | |
| 417-1 | 23 May 62 | Scout | Launch Failure Scout second stage exploded | |
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Personal Recollections Page |
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tangoz@zianet.com |
Don't forget to sign the guestbook and say hello. Last Updated Jan 29, 2000 |
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