HISTORY

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.

Early Program Chronology

19 Jul 61

Conditional approval to proceed with program planning

29 Jul 61

Satellite contract written and negotiated. Authority to proceed withheld pending successful booster negotiations.

21 Aug 61

Booster contracts completed. Approval to start work given to all contractors.

26 Oct 61

Unsatisfactory performance and schedule of NASA sponsored Scout fourth stage motor (ABL-258) noted at NASA-DOD coordination meeting

3 Nov 61

National range documentation completed entirely by program office

8 Nov 61

ABL-258 motor failed seventh time out of seven tests

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

25 Feb 62

Spacecraft prototype destroyed in vibration tests. Preliminary actions taken to terminate program. "Cure" notice sent contractor per ASPIR

13 Mar 62

Spacecraft structure redesign, refabrication and retest complete. Program back on schedule

2 Apr 62

MG-18 motor successfully fired in vacuum at Arnold Engineering Development Center

13 May 62

First 417 count-down scrubbed due to Scout hydraulic system failure

23 May 62

First 417 launch unsuccessful when Scout second stage exploded

23 Aug 62

Second launch attempt successful. Satellite operating normally in orbit

24 Oct 62

Authority to rebuild program peculiar ground stations received.

27 Oct 62

Direct readout station "Leda", in full operation at Eglin AFB

15 Nov 62

Third 417 booster and satellite placed in R-5 days stand-by status for indefinite period

26 Nov 62

Contractor started work on second set of four satellites

10 Dec 62

Discontinued operation of station "Leda" at Eglin AFB

17 Dec 62

total satellite capacity used for 24-hour period to give complete daylight map of Antarctica

19 Feb 63

Third 417 launch resulted in elliptical orbit due to poor third stage performance. Satellite operating normally

8 Mar 63

Fixed price contract for new ground stations issued to Radiation Incorporated following full competitive bid-evaluation board procedures

26 Apr 63

Fourth launch attempt failed with Scout third stage explosion

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)

14 Jun 63

Study of Scout reliability concludes primary cause of poor performance is poor program management by NASA. Extensive improvements recommended.

24 Jun 63

Patent disclosure filed by 417 Program Office on "DC motor" method of satellite spin control

1 Jul 63

On-orbit operations shifted to program peculiar ground stations and control center. Manning is 1200 per cent military

14 Aug 63

Logistics and maintenance support responsibility for 417 ground stations assumed by Air Force Logistics Command (AFLC) (SMAMA)

27 Sep 63

Fifth launch attempt failed with loss of Scout attitude control after third stage burn

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

31 Oct 63

Modified last three of current buy of six satellites to include DC spin control and other improvements

26 Nov 63

Directed to prepare plan using Thor/MG-18 booster configuration. Later nicknamed "Burner I."

23 Dec 63

Burner I plan approved. Implementation to be expedited

19 Jan 64

Satellites six and seven successfully launched from Thor-Agena. Both operating perfectly

7 Feb 64

Approval granted to kill satellite launch 19 Feb 63 since spin is too low to maintain altitude

17 Mar 64

Development of advanced IR system approved. Second Thor-Agena launch approved. Directed to proceed with System Definition Phase for Burner II

18 Jun 64

Second Thor-Agena launch placed spacecraft eight and nine in optimum orbit. Orbit velocity adjust included in F9

19 Jun 64

Per USWB request, procedures established to provide 417 data on tropical disturbances because Tiros data are inadequate. Code name, "Loose Talk"

28 Jul 64

Satellite F6 launched 19 Jan 64 killed because spin rate too low to operate

2 Sep 64

Fully funded fixed price contracts issued to Boeing Company and Ling-Temco-Vought for Phase I for Burner II

20 Nov 64

Directed to place tactical readout station near Saigon and to proceed to build special satellite (F15)

11 Jan 65

Directed to procure four more satellites with dual tactical/global capability (F16 through F19)

18 Jan 65

First Burner I launch carried satellite F10 to good orbit but satellite failed to separate form upper stage

28 Jan 65

Burner II Source Selection Board findings approved. Boeing will build stage

17 Mar 65

Satellite F7 launched 19 Jan 64 killed because spin rate too low to operate

18 Mar 65

Second Burner I launch placed F11 into good orbit. Satellite operating normally. Entire launch by military personnel

17 Apr 65

Tactical station at Tan Son Nhut Airfield completed and in operation

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


 
A launch history follows

 
 
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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