Delta II

In the early 1980s, all United States expendable launch vehicles were planned to be phased out in favor of the Space Shuttle, which would be responsible for all government and commercial launches. Production of Delta, Atlas-Centaur, and Titan 34D had ended. The Challenger disaster of 1986 and the subsequent halt of Shuttle operations changed this policy, and President Ronald Reagan announced in December 1986 that the Space Shuttle would no longer launch commercial payloads, and NASA would seek to purchase launches on expendable vehicles for missions that did not require crew or Shuttle support. McDonnell Douglas, at that time the manufacturer of the Delta family, signed a contract with the U.S. Air Force in 1987 to provide seven Delta II. These were intended to launch a series of Global Positioning System (GPS) Block II satellites, which had previously been manifested for the Space Shuttle. The Air Force exercised additional contract options in 1988, expanding this order to 20 vehicles, and NASA purchased its first Delta II in 1990 for the launch of three Earth-observing satellites. The first Delta II launch occurred on 14 February 1989, with a Delta 6925 boosting the first GPS Block II satellite (USA-35) from Launch Complex 17A (SLC-17A) at Cape Canaveral into a high medium Earth orbit. The first Delta II 7000-series flew on 26 November 1990, replacing the RS-27 engine of the 6000-series with the more powerful RS-27A engine. Additionally, the steel-cased Castor 4A solid boosters of the 6000-series were replaced with the composite-cased GEM 40. All further Delta II launches except three were of this upgraded configuration, and the 6000-series was retired in 1992 with the last launch being on July 24. McDonnell Douglas began Delta III development in the mid-1990s as increasing satellite mass required more powerful launch vehicles. The upgraded boosters would still find use on the Delta II, leading to the Delta II Heavy. On 28 March 2003, the Air Force Space Command began the process of deactivating the Delta II launch facilities and infrastructure at Cape Canaveral once the last of the second-generation GPS satellites were launched. However, in 2008, it instead announced that it would transfer all the Delta II facilities and infrastructure to NASA to support the launch of the Gravity Recovery and Interior Laboratory (GRAIL) in 2011. On 14 December 2006, with the launch of USA-193, was the first launch of the Delta II operated by United Launch Alliance. The last GPS launch aboard a Delta II and the final launch from SLC-17A at Cape Canaveral occurred in 2009. The GRAIL Launch in 2011 marked the last Delta II Heavy launch and the last from Florida. The final five launches would all be from Vandenberg Air Force Base in California. On 16 July 2012, NASA selected the Delta II to support the Orbiting Carbon Observatory (OCO-2), Soil Moisture Active Passive (SMAP), and Joint Polar Satellite System (JPSS-1 – NOAA-20) missions. This marked the final purchase of Delta II. OCO-2 was launched on 2 July 2014, Soil Moisture Active Passive (SMAP) was launched on 31 January 2015, and JPSS-1 was launched on 18 November 2017. All three of these launches were placed into orbit from SLC-2 at Vandenberg. The Delta II family launched 155 times. Its only unsuccessful launches were Koreasat 1 in 1995, and GPS IIR-1 in 1997. The Koreasat 1 launch was a partial failure caused by one booster not separating from the first stage, which resulted in the satellite being placed in a lower-than-intended orbit. By using reserve fuel, it was able to achieve its proper geosynchronous orbit and operated for 10 years. The GPS IIR-1 was a total loss as the Delta II exploded 13 seconds after launch. The explosion occurred when a damaged solid rocket booster casing ruptured and triggered the vehicle's flight termination system. No one was injured, and the launch pad itself was not seriously impacted, though several cars were destroyed and a few buildings were damaged. In 2007, Delta II completed its 75th consecutive successful launch, surpassing the 74 consecutive successful launches of the Ariane 4. With the launch of ICESat-2 in 2018, Delta II reached 100 consecutive successful launches. During its career, Delta II achieved a peak launch rate of 12 launches in a single year, although its infrastructure was capable of supporting up to 15 launches per year. == Vehicle description ==

First stage The first stage of the Delta II was propelled by a Rocketdyne RS-27 or RS-27A main engine burning RP-1 and liquid oxygen. This stage was technically referred to as the "Extra-Extended Long Tank Thor", a derivative of the Thor ballistic missile as were all Delta rockets until the Delta IV. The RS-27 used on the 6000-series Delta II produced of thrust, while the upgraded RS-27A used by the 7000-series produced . The stage was long and wide, had a mass of when fueled, and burned for 260 seconds. The GEM 40 boosters on the 7000-series further improved Delta II's performance by each featuring of extra propellant than the Castor 4A thanks to a lengthening of . In addition, the GEM boosters also boasted a lower dry mass than the Castors due to the former's carbon composite construction. In 2003, the Delta II Heavy debuted, featuring larger GEM 46 motors from the abandoned Delta III program. These new motors allowed the vehicle to carry over of extra payload into low-Earth orbit. Only Cape Canaveral Space Launch Complex 17B was capable of flying the Heavy configuration, as it was previously reinforced to handle the Delta III. This stage also contained a combined inertial platform and guidance system that controlled all flight events. The stage would also contain an S-band transmitter, batteries, and a sequencer to command the stage events. Two third-stage options were available, both consisting of a single solid rocket motor. The most common by far was Star 48, flying on over 70 missions. The Star 48, also referred to as the Payload Assist Module-Delta (PAM-D, PAM-Delta), was the more, powerful of the two options, producing an average thrust of about during its 87.1 seconds of burn time. The stage would end up flying primarily on the more powerful Delta variants and never flew on the three-booster configuration. The other third-stage option was Star 37FM. This stage flew four times, and only on three- and four-booster configurations of Delta. Star 37FM produced about of thrust during its 66.4-second burn. == Naming system ==

The Delta II family used a four-digit system to generate its technical names: • The first digit was either 6 or 7, denoting the 6000- or 7000-series Delta; • The second digit indicated the number of boosters. Most Delta II rockets flew with 9 boosters, but some flew with 3 or 4; • The third digit was always 2, denoting a second stage with an Aerojet AJ10 engine. Only Deltas prior to the 6000-series used a different engine, the TR-201; • The last digit denoted the third stage. 0 denoted no third stage, 5 indicated a Payload Assist Module (PAM) stage with Star 48B being used, and 6 indicated it used the Star 37FM motor for a PAM. • An H following the four digits denoted that the vehicle used larger Delta III GEM 46 boosters. The Heavy variant could be launched only from Cape Canaveral (as Vandenberg's pad wasn't modified to handle the larger SRBs) and was retired with the closure of that launch site in 2011; • Numbers and letters following those indicate the type of fairing. -9.5 means that the vehicle had a diameter fairing, -10 means an aluminum diameter fairing, -10C means a composite diameter fairing, and -10L indicates a lengthened diameter composite fairing. In some early Delta II flights, a fairing, about 8-feet in diameter (from older Delta rockets) was flown, and those vehicles had the -8 designation. For example, a Delta 7925H-10L used the RS-27A, nine GEM 46 boosters, a PAM third stage, and a lengthened diameter fairing. A Delta 6320–9.5 is a two-stage vehicle with an RS-27 first-stage engine, three Castor 4A boosters, a diameter fairing, and no third stage. == Launch profile ==

; Launch vehicle build-up: A Delta II launch vehicle was assembled vertically on the launch pad. Assembly started by hoisting the first stage into position. The solid rocket boosters were then hoisted into position and mated with the first stage. Launch vehicle build-up then continued with the second stage being hoisted atop the first stage. ; Fueling: It took approximately 20 minutes to load the first stage with of fuel. : At T-45 minutes, fueling completion was confirmed. At T-20 minutes, the FTS pyros were armed. At T-20 minutes and T-4 minutes, two built-in holds occurred. During these holds, final launch checkouts were performed. At T-11 seconds SRB igniters were armed. Ignition of the main engine was at T-0.4 seconds. The ascent profile varies between missions. ; SRB staging: If nine solid rocket boosters were used, only six were ignited at launch. After about a minute, once the first six were depleted, three air-start motors would ignite for another minute and the ground-start motors would separate. The air-start motors had nozzles optimized for high-altitude as they operated mostly in a near-vacuum during the flight. : If only three or four boosters were used, all were ignited on the ground and jettisoned at the same time. == Delta II launches ==

Notable payloads Earth-orbiting • GLAST • Gravity Probe B • 24 GPS satellites • 60 Iridium satellites • ICESat-2 • Kepler space telescope • OSTM/Jason-2 • Radarsat-1 • ELFIN • Polar (satellite) • ROSAT • STSS-ATRR • Swift • THEMIS • USA 193 (NROL-21) • WIND • WISE • WMAP • Geotail Interplanetary • 2001 Mars Odyssey • CONTOUR • Dawn • Deep Impact • Deep Space 1 • Genesis • GRAIL • Mars Climate Orbiter • Mars Exploration Rovers • Mars Global Surveyor • Mars Pathfinder • Mars Phoenix • Mars Polar Lander • MESSENGER • NEAR • Spitzer Space Telescope (SIRTF) • STEREO The last Delta II launch was the ICESat-2 satellite in September 2018. In 2008, ULA indicated that it had "around half a dozen" unsold Delta II rockets on hand, and by October 2017, ULA CEO Tory Bruno stated that there were no complete Delta II rockets left in ULA inventory. There were some unused Delta II components, but not enough to build another vehicle. A Delta II, made of these leftover parts alongside some simulated parts, is located at the Kennedy Space Center rocket garden. == Comparable rockets ==

• Antares • Ariane 4 (retired) • • Long March 4B • • Soyuz • (retired) • == Space debris ==

The only person on record ever hit by space debris, Lottie Williams, was hit by a small, light piece of a Delta II rocket. Williams was exercising in a park in Tulsa, Oklahoma on 22 January 1997 when she was hit in the shoulder by a piece of blackened metallic material. The U.S. Space Command confirmed that a used Delta II rocket from the April 1996 launch of the Midcourse Space Experiment had crashed into the atmosphere 30 minutes earlier. The object tapped her on the shoulder and fell off harmlessly onto the ground. Williams collected the item and NASA tests later showed that the fragment was consistent with the materials of the rocket, and Nicholas Johnson, the agency's chief scientist for orbital debris, believes that she was, indeed hit by a piece of a recently launched Delta II. Delta rockets have been involved in multiple fragmentation events as they were routinely left in orbit with enough fuel to explode. A large amount of current "space junk" is Delta rocket debris. == See also ==