Delta L

  • Castor 2 (3)
  • Long Tank Thor
  • Delta E
  • FW-4D
Launch historyStatusRetiredLaunch sitesCape Canaveral LC-17A
Vandenberg SLC-2ETotal launches2Success(es)1Failure(s)1First flight27 August 1969Last flight31 January 1972
[edit on Wikidata]

The Delta L, Thor-Delta L, or Thrust-Augmented Long Tank Thor-Delta was a US expendable launch system used to launch the Pioneer E and TETR satellites in 1969 (failed) and HEOS satellite in 1972. It was a member of the Delta family of rockets.

The Delta L was a three-stage rocket. The first stage was a Long Tank Thor, a stretched version of the Thor missile, augmented by three Castor-2 solid rocket boosters. The second stage was the Delta E. An FW-1D solid rocket motor was used as the third stage.

The first launch of the Delta L took place on 27 August 1969, from Launch Complex 17A at the Cape Canaveral Air Force Station. A defective valve caused plumbing in the hydraulics system to rupture and leak fluid, causing first-stage engine gimbaling to fail around 2+12 minutes into launch. The stage completed its burn successfully, but threw the second stage far off course. Orbital velocity could not be achieved, and Range Safety sent the destruct command at T+383 seconds. Neither the Pioneer E nor the TETR[1] payloads achieved orbit. The second, and final, Delta L launch was from Space Launch Complex 2E at the Vandenberg Air Force Base, on 31 January 1972. It successfully placed the HEOS-2 satellite into a highly elliptical orbit.[2][3]

References

  1. ^ Test satellite for NASA's Manned Space Flight Network see: http://www.astronautix.com/t/tetr.html
  2. ^ Wade, Mark. "Delta". Archived from the original on 2008-07-24.
  3. ^ Krebs, Gunter. "Thor Family". Gunter's Space Page. Archived from the original on 2007-08-06. Retrieved 2021-12-21.
  • v
  • t
  • e
Orbital launch systems
Current
In developmentRetired
Classes
  • This Template lists historical, current, and future space rockets that at least once attempted (but not necessarily succeeded in) an orbital launch or that are planned to attempt such a launch in the future
  • Symbol indicates past or current rockets that attempted orbital launches but never succeeded (never did or has yet to perform a successful orbital launch)
  • v
  • t
  • e
Orbital launch systems developed in the United States
Active
In development
Retired
  • * - Japanese projects using US rockets or stages
  • ** - uses Russian engines
  • - never succeeded
  • †† - no new orders accepted
  • ††† - used Ukrainian first stage
  • v
  • t
  • e
Thor and Delta rockets
Rockets
Thor
Delta
Alphabetical
Numerical
Modern
Export
Launch sites
Canaveral
Johnston
  • LE-1
  • LE-2
Tanegashima
Vandenberg
Bases
Components
Boosters
First stages
Upper Stages
Delta
Other
  • Able
  • Ablestar
  • Agena
  • Altair
  • Burner
  • FW-4D
  • IABS
  • PAM-D
  • Star
  • UM-129
Engines
Manufacturers
Rocket
Engines
Launches
  • 1957–1959
  • 1960–1969
  • 1970–1979
  • 1980–1989
  • 1990–1999
  • 2000–2009
  • 2010–2019
  • 2020–2024


Stub icon

This rocketry article is a stub. You can help Wikipedia by expanding it.

  • v
  • t
  • e