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Atlas Burner 2
Part of Atlas
American orbital launch vehicle. Atlas SLV-3 + 1 x Star 37B upper stage.
Status: Retired 1972. First Launch: 1968-08-16. Last Launch: 1972-10-02. Number: 2 . Thrust: 1,700.00 kN (382,100 lbf). Gross mass: 130,000 kg (280,000 lb). Height: 28.90 m (94.80 ft). Diameter: 3.05 m (10.00 ft). Apogee: 800 km (490 mi).
More at: Atlas Burner 2.
Family:
orbital launch vehicle.
Country:
USA.
Spacecraft:
Calsphere,
OV5,
Orbiscal,
RADCAT,
RM,
Radsat.
Launch Sites:
Vandenberg,
Vandenberg SLC3E,
Vandenberg 576A1.
Stages:
Atlas Agena SLV-3,
Atlas MA-5A,
Star 37B.
Agency:
Convair.
1968 August 16 - .
20:57 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas.
Launch Vehicle:
Atlas Burner 2.
FAILURE: Failure.
Failed Stage: 1.
- LCS 3 - .
Payload: LCS 3. Mass: 37 kg (81 lb). Nation: USA.
Agency: USAF,
USN.
Class: Earth.
Type: Ionosphere satellite. Spacecraft: Orbiscal.
Decay Date: 1968-08-16 .
An Atlas/Burner II (SLV-3, #7004), the first Atlas to be launched with a Burner II upper stage, was launched from Space Launch Complex 3 East (SLC-3E) at Vandenberg but failed to place its payload in orbit due to a malfunction of the nose-fairing heat shield separation system. First of two Atlas/Burner II space launches. 1 of 13 satellite launch attempts; investigate effects of ionosphere on radio signals.
- AVL-802 Rigid Sphere - .
Payload: AVL-802. Nation: USA.
Agency: USAF AFSC.
Spacecraft: Calsphere.
An Atlas/Burner II (SLV-3, #7004), the first Atlas to be launched with a Burner II upper stage, was launched from Space Launch Complex 3 East (SLC-3E) at Vandenberg but failed to place its payload in orbit due to a malfunction of the nose-fairing heat shield separation system.
- LIDOS - .
Payload: LIDOS. Mass: 37 kg (81 lb). Nation: USA.
Agency: USAF AFSC.
Spacecraft: Orbiscal.
- Orbiscal 1 - .
Payload: Orbiscal 1. Mass: 37 kg (81 lb). Nation: USA.
Agency: USAF AFSC.
Spacecraft: Orbiscal.
- Radcat - .
Payload: Radcat. Mass: 208 kg (458 lb). Nation: USA.
Agency: USAF AFSC.
Spacecraft: Radcat.
- RM-18 - .
Payload: RM-18. Mass: 46 kg (101 lb). Nation: USA.
Agency: USAF AFSC.
Spacecraft: RM.
- AVL-802 Grid Sphere 7-1 - .
Payload: AVL-802. Mass: 37 kg (81 lb). Nation: USA.
Agency: USAF AFSC.
Spacecraft: Orbiscal.
- EGRS 11 - .
Payload: EGRS 11. Mass: 37 kg (81 lb). Nation: USA.
Agency: USAF AFSC.
Spacecraft: Orbiscal.
- EGRS 12 - .
Payload: EGRS 12. Mass: 37 kg (81 lb). Nation: USA.
Agency: USAF AFSC.
Spacecraft: Orbiscal.
1972 October 2 - .
20:09 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A1.
LV Family:
Atlas.
Launch Vehicle:
Atlas Burner 2.
- RADCAT - .
Payload: Radsat / Radcat / OPS 8180. Mass: 208 kg (458 lb). Nation: USA.
Agency: US Army.
Class: Technology.
Type: Military technology satellite. Spacecraft: RADCAT.
Decay Date: 2012-08-02 . USAF Sat Cat: 6212 . COSPAR: 1972-076A. Apogee: 638 km (396 mi). Perigee: 627 km (389 mi). Inclination: 98.60 deg. Period: 97.40 min.
An Atlas F/Burner IIA launch vehicle, carrying SAMSO's Space Test Program Flight 72-1, was launched from Vandenberg. This was the first use of this booster/upper stage combination. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).
- Radsat - .
Payload: P 72-1 / OPS 8180. Mass: 726 kg (1,600 lb). Nation: USA.
Agency: USAF.
Class: Technology.
Type: Military technology satellite. Spacecraft: Radsat.
USAF Sat Cat: 6217 . COSPAR: 1972-076B. Apogee: 705 km (438 mi). Perigee: 688 km (427 mi). Inclination: 98.70 deg. Period: 98.70 min.
An Atlas F/Burner IIA launch vehicle, carrying SAMSO's Space Test Program Flight 72-1, was launched from Vandenberg. This was the first use of this booster/upper stage combination. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).
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