Thor-Agena
| Status | Retired |
|---|---|
| Country | United States |
| Manufacturer | Douglas |
| Number of orbital launches | 185 |
| First launch | 1959-02-28 |
| Last launch | 1972-05-25 |
Launches by year:
Latest launches:
| Launch date | Launch site | Rocket / Variant | Payload | Notes | Status |
|---|---|---|---|---|---|
| 1972-05-25 | Vandenberg | Thor-Agena Thorad SLV-2H Agena D | KH-4B 17 | success | |
| 1972-04-19 | Vandenberg | Thor-Agena Thorad SLV-2H Agena D | KH-4B 16 | success | |
| 1971-12-14 | Vandenberg | Thor-Agena Thorad SLV-2G Agena-D | Poppy 9A / Poppy 9B / Poppy 9C / Poppy 9D | success | |
| 1971-10-17 | Vandenberg | Thor-Agena Thorad SLV-2G Agena-D | ASTEX (P71-2) | success | |
| 1971-09-10 | Vandenberg | Thor-Agena Thorad SLV-2H Agena D | KH-4B 15 / Arroyo | success | |
| 1971-07-16 | Vandenberg | Thor-Agena Thorad SLV-2H Agena D | Strawman 4 & RM 19 | success | |
| 1971-03-24 | Vandenberg | Thor-Agena Thorad SLV-2H Agena D | KH-4B 14 | success | |
| 1971-02-17 | Vandenberg | Thor-Agena Thorad SLV-2H Agena D | KH-4B 13 / P-801 3 | failure | |
| 1970-11-18 | Vandenberg | Thor-Agena Thorad SLV-2H Agena D | KH-4B 12 / Tophat 1 | success | |
| 1970-08-26 | Vandenberg | Thor-Agena Thorad SLV-2G Agena-D | Strawman 3 | success | |
| + 175 more... | |||||
Variants:
(This section is under construction)Thor-Agena Thor DM-18A Agena A
| First launch | 1959-02-28 |
|---|---|
| Stages | 2 |
| Boosters | 0 |
| Mass | 53.13 t |
| Height | 28 m |
1959 saw the introduction of another series of two-stage carrier rockets based on Thor: Thor-Agena. This incorporated Lockheed’s RM-81 Agena vehicle which was designed to serve both as part of the rocket and a general-purpose platform upon which satellites could be constructed
Thor-Agena Thor SLV-2 Agena-B (Thor DM-21 Agena B)
| First launch | 1960-10-26 |
|---|---|
| Stages | 2 |
| Boosters | 0 |
| Mass | 56.51 t |
| Height | 31 m |
Payload capacity:
| LEO | 400 kg to 1,100 km / 100 deg |
|---|
Incorporated an upgraded version of Agena, the Agena-B, with stretched propellant tanks and a restartable engine, and the upgraded DM-21 first stage.
Thor-Agena Thor SLV-2 Agena-D (Thor DM-21 Agena D)
| First launch | 1962-06-28 |
|---|---|
| Stages | 2 |
| Boosters | 0 |
| Mass | 56.51 t |
| Height | 31 m |
Thor-Agena Thor SLV-2A Agena D (TAT Agena D)
| First launch | 1963-02-28 |
|---|---|
| Stages | 2 |
| Boosters | 3 x Thiokol Castor TX-345-5 |
| Mass | 67.82 t |
| Height | 31 m |
Thor-Agena Thor SLV-2A Agena-B (TAT Agena B)
| First launch | 1963-06-29 |
|---|---|
| Stages | 2 |
| Boosters | 3 x Thiokol Castor TX-345-5 |
| Mass | 67.5 t |
| Height | 31 m |
The Thrust-Augmented Thor (TAT) incorporated three Castor-1 solid rocket motors (SRMs) clustered around the base of the vehicle. These provided additional thrust at liftoff, increasing the rocket’s payload capacity.
Thor-Agena Thorad SLV-2G Agena-D
| First launch | 1966-08-09 |
|---|---|
| Stages | 2 |
| Mass | 91.4 t |
| Height | 32.9 m |
Thor-Agena Thorad SLV-2H Agena D
| First launch | 1969-06-05 |
|---|---|
| Stages | 2 |
| Mass | 88.73 t |
| Height | 34 m |
