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At request of Army Ordnance, Cal Tech's rocket laboratory developed the first US long-range missiles. Project ORDCIT resulted in development of the Private A and Corporal missiles. At Camp Irwin, Calif., 24 Private A rockets were launched by JPL, only 11 months after the start of Project ORDCIT. This rocket technology that led to later operational Corporal and Sergeant missiles.

From 1960 to 1961 Korolev's design bureau worked on this single stage military rocket. The 25 tonne missile could hurl an 800 kg warhead over a 2300 km range. It was powered by a single-chamber engine using AK-270/TM-185 storable propellants. The rocket featured automatic guidance, instantaneous launch capability, and was air-transportable. Both mobile and fixed versions were designed, and the small missile was easy to camouflage. Korolev completed work in September 1961. A competing missile was selected for the requirement.

United Arab Republic neither confirmed nor denied reports of November 8 that it had successfully launched its first rocket. Dr. Eugen Saenger of the Stuttgart Jet Propulsion Institute in Germany denied any connection with the United Arab Republic program as charged by Israel.

The RT-1 was an experimental solid propellant ballistic missile. A decree of 20 November 1959 authorised Korolev to begin development of the three stage rocket, which was to have a range of 800 to 2500 km and a lift-off mass of 35 tonnes. Soviet solid rocket motor technology of the time meant that each stage of the vehicle was composed of bundles of four 800 mm diameter solid rocket motors of varying lengths. The rocket was launched from a tube and arced over to a forty-five degree angle as soon as it cleared the launch tube. Air vanes provided steering for the second stage. First flight was on 28 April 1962. Work was completed at the end of 1965

Development of the RT-2 ICBM was authorised by a decree of 4 April 1961 in parallel with the RT-1. Korolev completed the draft project in March 1963. The modular design had three stages, each with three nozzles. The first stage had a thrust of 88 tonnes; the second 33 tonnes; and the third 14 tonnes. Three missiles could be derived from these stages, using a common guidance system. The 8K96 IRBM used stages 2 and 3; it was not put into production. The 8K97 IRBM used stages 1 and 3; this went into service in 1968. The 8K98 ICBM used all three stages and was deployed in limited numbers for over twenty years.

Italy briefly flirted with the creation of an independent nuclear deterrent in the late 1960's. The Alfa project for an indigenous Italian submarine- and ship-launched ballistic missile was begun in 1971. Three Alfa test missiles with inert second stages were successfully launched in 1975-1976 from Salto di Quirra in Sardinia. The programme was abandoned at this stage, when Italy and its neighbours ratified the nuclear proliferation treaty.

The Yangel MR-UR-100 was designed as a replacement for Chelomei's UR-100 at the end of its 10 year storage life. Although it could be installed in the same silos, it was 50% heavier. The competing design of Chelomei, the UR-100N, was also put into production when the Soviet hierarchy deadlocked and could not pick one design over the other.

Burlak air-launched satellite launcher was proposed in 1992 and studied by Germany in 1992-1994. Evidently based on secret anti-satellite missile. Air launched from Tu-160 bomber, released at 13,500 m altitude and Mach 1.7. Development estimated to cost only DM 50 million, but not proceeded with. Burlak/Diana variant would have been launched from Concorde.

As of January 2000, the Shahab-4, if still an active project, had not entered flight test stage.