Titan 23G
The Titan 23G, Titan II(23)G, Titan 2(23)G or Titan II SLV was an American medium-lift launch vehicle derived from the LGM-25C Titan II intercontinental ballistic missile. Retired Titan II missiles were converted by Martin Marietta, into which the Glenn L. Martin Company, which built the original Titan II, had merged. It was used to carry payloads for the United States Air Force (USAF), NASA and National Oceanic and Atmospheric Administration (NOAA).
Also recorded as Titan II(23)G · Titan 2(23)G · Titan II SLV · Titan II Space Launch Vehicle
Titan 23G

US Air Force · Public domain
- Name
- Titan 23G
- Field
- LGM-25C Titan II.
- Region
- United States.
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Documentary summary
The Titan 23G, Titan II(23)G, Titan 2(23)G or Titan II SLV was an American medium-lift launch vehicle derived from the LGM-25C Titan II intercontinental ballistic missile. Retired Titan II missiles were converted by Martin Marietta, into which the Glenn L. Martin Company, which built the original Titan II, had merged. It was used to carry payloads for the United States Air Force (USAF), NASA and National Oceanic and Atmospheric Administration (NOAA).
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wikidata · Q5918827 · wikipedia · Titan 23G
In this article
Overview
Overview
Thirteen were launched from Space Launch Complex 4W (SLC-4W) at the Vandenberg Air Force Base between 1988 and 2003.
Key facts
Key facts
• Name — Titan 23G • Function — Medium-lift launch vehicle • Manufacturer — Martin Marietta / Lockheed Martin • Country Origin — United States • Stages — 2 or 3 • Status — Retired • Family — Titan • Sites — Vandenberg, SLC-4W • First — 5 September 1988 • Last — 18 October 2003 • Launches — 13 • Success — 12 • Fail — 1 • Payloads — Clementine QuickSCAT
Configuration
Configuration
Titan 23G rockets consisted of two stages burning liquid propellant. The first stage was powered by one Aerojet LR87 engine with two combustion chambers and nozzles, and the second stage was propelled by an LR91. On some flights, the spacecraft included a kick motor, usually the Star-37XFP-ISS; however, the Star-37S was also used. A contract to refurbish fourteen Titan II missiles to the Titan 23G configuration was awarded to Martin Marietta in January 1986. The first launch occurred on 5 September 1988, carrying a classified payload for the U.S. National Reconnaissance Office. Thirteen were launched, with the fourteenth going to the Evergreen Aviation Museum. The final flight occurred on 17 October 2003, carrying a Defense Meteorological Satellite Program (DMSP) satellite. During refurbishment, the forward structure of the second stage was modified with the addition of a payload attachment fitting to attach the payload to the rocket, and installing a payload fairing to protect it during launch. The engines were refurbished, and the rockets' guidance and control systems were upgraded by Delco Electronics. The former Titan IIIB pad at Vandenberg, SLC-4W, was modified to accommodate the Titan 23G, and was used for all thirteen launches.
Launch history
Launch history
All launches of Titan II(23)G rockets took place from Space Launch Complex 4W (SLC-4W) at Vandenberg Air Force Base. • Date/Time (UTC) — Serial number — Third Stage — Payload — Outcome — Remarks • Rocket — Stages • 5 September 1988 09:25 — G-1 — B-98/56 — None — USA-32 (Bernie) FARRAH III — • 6 September 1989 01:48 — G-2 — B-75/99 — None — USA-45 (Bernie) FARRAH IV — Spacecraft failed immediately after launch • 25 April 1992 08:53 — G-3 — B-102 — None — USA-81 (Bernie) FARRAH V • 5 October 1993 17:56 — G-5 — B-65 — Star-37XFP-ISS — Landsat 6 — Star-37 failure, spacecraft failed to achieve orbit • 25 January 1994 16:34 — G-11 — B-89/67 — None — Clementine DSPSE-ISA — • 4 April 1997 16:47 — G-6 — B-106 — Star-37S-ISS — USA-131 (DMSP-5D2 F-14) — • 13 May 1998 15:52:04 — G-12 — B-84/80 — Star-37XFP-ISS — NOAA-15 (NOAA-K) — Included oxidizer (N 2 O 4) tank from Titan II B-72 • 20 June 1999 02:15:00 — G-7 — B-99/75 — None — QuikSCAT — • 12 December 1999 17:36:01 — G-8 — B-94/44 — Star-37XFP-ISS — USA-147 (DMSP-5D3 F-15) — • 21 September 2000 10:22 — G-13 — B-96/39 — Star-37XFP-ISS — NOAA-16 (NOAA-L) — • 24 June 2002 18:23:04 — G-14 — B-71/72 — Star-37XFP-ISS — NOAA-17 (NOAA-M) — Included oxidizer tank from Titan II B-92 • 6 January 2003 14:19 — G-4 — B-105 — None — Coriolis — • 18 October 2003 16:17 — G-9 — B-107 — Star-37XFP-ISS — USA-172 (DMSP-5D3 F-16) — Final Titan II launch
Remaining rockets
Remaining rockets
• Illustration — Titan-II B-108 in 1988 became Titan-23G10 program spare • Illustration — Titan-23G10 at the Evergreen Aviation & Space Museum A fourteenth rocket, G-10, based on Titan II B-108, but incorporating an oxygen tank from B-80, was not launched and is preserved at the Evergreen Aviation & Space Museum in McMinnville, Oregon. The remaining 42 Titan II missiles were stored at Davis-Monthan AFB with most being broken up for salvage. Four were transferred to museums.
Classification and Refurbishment History
Classification and Refurbishment History
English Wikipedia and records from Wikidata document that the Titan 23G is classified as an American expendable space launch vehicle derived directly from the LGM-25C Titan II intercontinental ballistic missile. The original LGM-25C Titan II missiles were manufactured by the Glenn L. Martin Company, which subsequently merged into Martin Marietta. In January 1986, Martin Marietta received a contract from the United States military to refurbish fourteen decommissioned Titan II missiles into the Titan 23G launch vehicle configuration. The conversion process required structural and systems modification of the surplus airframes. According to English Wikipedia summaries, Martin Marietta altered the forward structure of the second stage by adding a payload attachment fitting to secure spacecraft to the vehicle, alongside a newly installed payload fairing to protect satellite payloads during ascent through the atmosphere. The rocket engines were completely refurbished, while Delco Electronics upgraded the vehicle guidance and control systems. The remaining forty-two Titan II missiles were sent to Davis-Monthan Air Force Base, where most were broken up for salvage and four were transferred to museum holdings.
Surplus Disposition and Museum Holdings
English Wikipedia records that the Titan 23G—variously designated in historical listings as the Titan II(23)G, Titan 2(23)G, and Titan II Space Launch Vehicle—was an American medium-lift launch vehicle adapted from retired LGM-25C Titan II intercontinental ballistic missiles. The original intercontinental missiles were produced by the Glenn L. Martin Company, which subsequently merged into Martin Marietta. In January 1986, Martin Marietta received a contract to refurbish fourteen decommissioned Titan II airframes into the space launch configuration. Refurbishment entailed substantial modifications to the second stage forward structure, including the addition of a payload attachment fitting and a protective payload fairing for ascent. According to English Wikipedia, the liquid-propellant engines underwent refurbishment, whilst Delco Electronics performed upgrades upon the guidance and control systems. Space Launch Complex 4W at Vandenberg Air Force Base, formerly utilised for Titan IIIB operations, was reconfigured specifically to support the launch vehicle. English Wikipedia notes that thirteen Titan 23G rockets were launched from Space Launch Complex 4W between 1988 and 2003, deploying payloads on behalf of the United States Air Force, NASA, and the National Oceanic and Atmospheric Administration. The inaugural flight took place on 5 September 1988, placing a classified payload into orbit for the United States National Reconnaissance Office. The final launch occurred on 17 October 2003, carrying a Defense Meteorological Satellite Program payload. Propulsive assemblies across the series comprised a two-stage liquid-propellant configuration, consisting of a first stage driven by an Aerojet LR87 engine with two combustion chambers and nozzles, and a second stage propelled by an Aerojet LR91 engine, as documented in authority records maintained by Wikidata and English Wikipedia. On select missions, upper-stage propulsion was augmented by a kick motor, predominantly the Star-37XFP-ISS, though the Star-37S variant was also employed. Regarding surplus disposition, English Wikipedia indicates that out of the fourteen airframes refurbished under the 1986 contract, thirteen completed operational flights, leaving a single vehicle unlaunched. Designated G-10, this fourteenth airframe was constructed from Titan II airframe B-108 and integrated with an oxygen tank retrieved from airframe B-80. Rather than undergoing launch, vehicle G-10 was transferred to public display and is preserved at the Evergreen Aviation & Space Museum in McMinnville, Oregon. The remaining forty-two surplus Titan II missiles not designated for the refurbishment programme were transferred to storage at Davis-Monthan Air Force Base. English Wikipedia records that the majority of these stored airframes were subsequently broken up for salvage, while four airframes were transferred to museum collections for preservation. The physical criteria for distinguishing converted Titan 23G structures from unmodified Titan II airframes in museum holdings are not established in the supplied evidence. Furthermore, no evidence is provided regarding the formal valuation, market status, or legal disposition of the surviving salvageable airframes and components stored at Davis-Monthan Air Force Base.
Notes from the source article
Cited by Wikipedia
Notes from the source article
These works are cited by the source article, in its own numbering. They are recorded as its citations, not as sources VALÉORINE has verified.
- 1.Krebs, Gunter. Titan-2. Gunter's Space Page.
- 2.Kyle, Ed. Titan 23G Data Sheet. Space Launch Report. 2009-04-14.
- 3.Wade, Mark. Titan. Encyclopedia Astronautica.
- 4.Krebs, Gunter Dirk. Titan-2(23)G Star-37XFP-ISS (Titan-2G Star-37XFP-ISS). Gunter's Space Page.
- 5.Wade, Mark. Landsat 6. Encyclopedia Astronautica.
- 6.Krebs, Gunter Dirk. DSPSE-ISA. Gunter's Space Page.
- 7.Krebs, Gunter Dirk. Titan-2(23)G Star-37S-ISS (Titan-2G Star-37S-ISS). Gunter's Space Page.
References
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1- LGM-25C Titan IITerminology
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The Titan 23G rocket architecture comprised a two-stage liquid-propellant design incorporating specific propulsion assemblies recorded in Wikidata authority files. English Wikipedia records indicate that the primary stage was powered by a single Aerojet LR87 liquid-fuelled rocket engine equipped with two distinct combustion chambers and exhaust nozzles. The second stage utilised an Aerojet LR91 liquid-propellant engine to provide upper-stage acceleration following first-stage separation. Both main engines underwent complete refurbishment during the vehicle transformation process carried out under contract by Martin Marietta. For missions requiring additional orbital insertion capability, the vehicle could be configured with an optional third-stage solid kick motor. Wikipedia records document that these flights incorporated either a Star-37XFP-ISS or a Star-37S solid-propellant motor, situated above the second stage within the payload compartment. Recorded constituent parts for the overall launch vehicle assembly include the LR-87, LR-91, and Star 37 propulsion units. The physical integration of these engines within the modified second-stage forward structure ensured compatibility with various governmental satellite payloads. Physical criteria for distinguishing converted Titan 23G structures from unmodified Titan II airframes in museum holdings are not established in the available evidence.
All operational flights of the Titan 23G were conducted from Space Launch Complex 4W (SLC-4W) at Vandenberg Air Force Base in California. English Wikipedia notes that SLC-4W, previously utilised as a Titan IIIB launch pad, was specifically modified to accommodate the Titan 23G configuration. Between 1988 and 2003, a total of thirteen Titan 23G vehicles were successfully launched from this facility to place government payloads into earth orbit. The operational history of the vehicle commenced on 5 September 1988 with the launch of a classified payload for the U.S. National Reconnaissance Office. Over its fifteen-year service life, the rocket carried spacecraft for the United States Air Force, NASA, and the National Oceanic and Atmospheric Administration. The final flight occurred on 17 October 2003, deploying a Defense Meteorological Satellite Program satellite for atmospheric observation. The non-operational airframe designated G-10 remained unlaunched and was subsequently transferred to the Evergreen Aviation & Space Museum in McMinnville, Oregon. The formal valuation, market status, or legal disposition of surviving salvageable airframes stored at Davis-Monthan Air Force Base is not established in the supplied records.
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