The Thor DSV-2U or Thor LV-2F Star-37XE Star-37S-ISS was an American expendable launch system used to launch five DMSP weather satellites between 1976 and 1980.[1][2] It was a member of the Thor family of rockets, and a derivative of the Thor DSV-2.[1][3]

Launch of the last Thor DSV-2U carrying DMSP-5D1 F5
FunctionExpendable launch system
Country of originUnited States
Size
Mass49500 kg
Stages3
Capacity
Payload to LEO500 kg
Launch history
StatusRetired
Launch sitesVandenberg SLC-10W
Total launches5
Success(es)4
Failure(s)1
First flightSeptember 11 1976
Last flightJuly 15 1980
First stage - Thor DM-19
EnginesLR79-7
Thrust758.71 kN
Specific impulse282
Burn time165
PropellantLOx/Kerosene
Second stage Star 37XE
EnginesTE-M-714-4
Thrust45 kN
Burn time66
Propellantsolid
Third stage - Star-37S-ISS
EnginesTE-M-364-15
Thrust51.1 kN
Burn time60
Propellantsolid

The first stage was a Thor missile in the DM-19 configuration. A Star-37XE was used as the second stage, and the third stage was a Star-37S-ISS.

Thor boosters used an erector system to hoist them up to the pad. While common on Soviet launch vehicles, this method was unusual in the US space program.

Launches

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Thor DSV-2U was launched five times between 1976 and 1980 from Space Launch Complex 10W at the Vandenberg Air Force Base.[1][2]

All launches carried DMSP 5D-1 satellites The final launch (Thor 304) occurred on July 14, 1980 and was a failure.

Thor DSV-2U launches[1][2]
Serial Number Launch date Name Status
172 11 Sep 1976 DMSP 5D-1/F1 In orbit; aka AMS 1
183 5 Jun 1977 DMSP 5D-1/F2 In orbit; aka AMS 2
143 1 May 1978 DMSP 5D-1/F3 In orbit; aka AMS 3
264 6 Jun 1979 DMSP 5D-1/F4 In orbit; aka AMS 4
304 14 July 1980 DMSP 5D-1/F5 Failed to orbit; aka AMS 5

Thor 304 failure

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Thor 304 had been erected on the pad a few weeks before launch, and during this step, a connecting pin in the erector broke and sent the rocket falling back down to ground level. Launch crews examined the Thor for damage, but could not find any outward indication of it. The booster passed routine preflight systems checks and liftoff took place at 6:22 PM PST on July 14, 1980.

Shortly after liftoff, the Thor's telemetry system failed, but weather conditions and visibility were excellent, and the booster could be tracked visually for over two minutes. Telemetry from the DMSP satellite indicated that it was operating properly. SECO took place on time, as did the second stage burn. Third stage burn began, and then after about four seconds, all telemetry abruptly ceased.

The initial assumption was that the third stage exploded, and initial Air Force press releases about the launch stated such. However, radar tracking showed that the third stage motor continued operating as it drove the DMSP into the Pacific Ocean.

The investigation board concluded that connectors in the electrical interface between the second and third stage had been jolted loose by the erector mishap several weeks earlier. After second stage burnout, staging failed to take place due to the misaligned connectors, and the third stage motor thus fired with the spent second stage still attached to it. The force from the third stage motor burning managed to tear the second stage free, but in doing so, it ripped out wiring in the base of the third stage, which shorted out the guidance computer and caused it to direct the stage and spacecraft down into the ocean. Much like the DMSP failure in 1976, the incident was attributed to poor program management.[4]

References

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  1. ^ a b c d "Thor-LV2F Star-37XE Star-37-S-ISS". Gunter's Space Page. Retrieved 2024-04-12.
  2. ^ a b c "Thor DSV-2U". www.astronautix.com. Retrieved 2024-10-11.
  3. ^ Wade, Mark (2013-08-17). "Delta". Archived from the original on 2013-08-17. Retrieved 2024-04-12.
  4. ^ "The Space Review: Launch failures: Two Thors, one problem".