пакетная схема Р-7 · 1947–1957

R-7 packet scheme

R-7의 패킷 방식

A Soviet rocket design approach in which multiple stages are arranged in parallel, not in series, with all engines ignited simultaneously on the ground. First proposed by Mikhail Tikhonravov at NII-4 in 1947 and presented in July 1948 as 'Paths to Achieving Long Ranges with Ballistic Rockets,' it was refined through Dmitry Okhotsimsky's mathematical optimisation (1951) and Helmut Gröttrup's G-5 concept. By sidestepping the unsolved problem of in-flight air-start ignition of large engines, the packet scheme made a practical ICBM feasible and became the structural basis of the R-7 and its descendants.

In depth

Origins: Tikhonravov and the 'Rocket Packet'

The theoretical origin of the packet scheme lies in Konstantin Tsiolkovsky's 'rocket squadron' (эскадра ракет) concept, sketched in his 1935 work 'The Maximum Speed of a Rocket.' Tsiolkovsky envisioned multiple rockets flying together with only hydraulic connections, but it was Mikhail Tikhonravov who turned this into an engineering design.

In 1947, Tikhonravov, then deputy director of NII-4, began investigating parallel staging to solve two structural problems with sequential staging: the unsolved challenge of air-starting a second-stage engine in flight, and the impractically enormous length of a single very large rocket. His concept was to mechanically join several identical rockets into one 'packet,' ignite all engines simultaneously on the ground, and sequentially drain and jettison the outer rockets.

On 14 July 1948, Tikhonravov delivered an expanded report titled 'Paths to Achieving Long Ranges with Ballistic Rockets' at the Academy of Artillery Sciences. He argued that a packet scheme could theoretically achieve unlimited range and even place an artificial satellite into orbit. The audience was hostile. His department was disbanded as 'pursuing irrelevant problems' and Tikhonravov himself was demoted from deputy director to scientific consultant.

Korolev's Intervention and Okhotsimsky's Optimisation

Sergei Korolev recognised the concept's potential immediately upon reading Tikhonravov's report. In December 1949, he issued an official contract to NII-4 for 'Research on the feasibility and advisability of creating packet-type long-range composite rockets,' reviving Tikhonravov's team. In March 1950, Tikhonravov's second report, 'Rocket Packets and Prospects for Their Development,' demonstrated that a two-stage packet of three R-2-class rockets could deliver a heavy warhead over intercontinental distances.

Korolev favoured a central core with four boosters over the simpler three-rocket packet and commissioned the Steklov Mathematical Institute's Department of Applied Mathematics, led by Dmitry Okhotsimsky, to optimise it. In 1951, Okhotsimsky's team produced a general study of sequential and parallel staging, including fuel transfer between stages, providing the mathematical foundation for the R-7's exact booster proportions and geometry.

Gröttrup's G-5 and the German Contribution

Helmut Gröttrup's German rocket team, confined on Gorodomlya Island, independently developed a similar parallel-staging concept between 1947 and 1949: the G-5, a bundle of multiple G-4-class rockets. This is considered a direct ancestor of the R-7, and the tapered conical booster shape that persisted through Soyuz variants was first proposed by the German team in 1949. For political reasons, the German contribution was long minimised, but contemporary scholarship recognises a triple lineage of Tikhonravov–Okhotsimsky–Gröttrup as the packet scheme's true origin.

Core Design Principle and Historical Significance

The packet scheme's decisive advantage was that all first-stage engines ignited on the ground, completely bypassing the unsolved technical challenge of high-altitude air-start ignition. The core's RD-108 and the four boosters' RD-107 engines, totalling 20 combustion chambers, all fired simultaneously on the launch pad; the boosters separated after approximately 120 seconds upon propellant depletion. This was the only feasible ICBM design path at the time. Although the R-7 was soon obsolete as a weapon, it became the foundation of the Sputnik, Vostok, and Soyuz launch vehicle families.

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Sources

  1. Wikipedia (EN) In 1947, Mikhail Tikhonravov developed a theory of parallel stages he called 'packet rockets'; three parallel stages fired from liftoff with fuel drawn from outer stages first; in 1951 Dmitry Okhotsimsky carried out pioneering study of sequential and parallel staging; design of R-7 Semyorka emerged from that study
  2. Wikipedia (EN) The principle of a staged missile, also known as a 'rocket packet,' was first proposed by Mikhail Tikhonravov at NII-4 in 1947; Korolev became aware in 1948; further refined by Okhotsimsky's Department of Applied Mathematics in 1951
  3. Wikipedia (RU) Первопричиной создания МБР Р-7 стала работа 1947–1948 гг. группы М. К. Тихонравова в НИИ-4 по применению 'пакетной' схемы; 14 июля 1948 г. Тихонравов выступил с докладом 'Пути осуществления больших дальностей стрельбы ракетами'; оптимальной представлялась ракета 'пакетной' схемы из центрального блока и четырёх боковых
  4. document.wikireading.ru Detailed history of Tikhonravov's packet scheme: idea origins in Tsiolkovsky's 'rocket squadron'; 1947 manual calculations at NII-4; 14 July 1948 landmark report; hostile reception and Tikhonravov's demotion; Korolev's December 1949 rescue contract; March 1950 second report 'Rocket Packets and Prospects'
  5. drewexmachina.com Genesis of R-7 design traced to Tikhonravov's 'Rocket Packet' proposal of mid-1947; parallel staging with cluster of five rockets ignited simultaneously at liftoff; from 1949–1951 MIAN under Keldysh did detailed studies; led to T-1 design study
  6. Wikipedia (EN) G-5/R-15 ICBM designed by Groettrup team using 'packet of G-4s' was direct ancestor of Korolev's R-7; launcher for Sputnik based on R-7 with bundling (packeting) of 20 engines with conical rocket bodies as proposed by German scientists in 1949
  7. Wikipedia (EN) Okhotsimsky studied parallel 'packet' rockets and schemes involving pumping of fuel between stages during flight; this led directly to the design of the R-7 missile and the exact proportions of its strap-on booster stages
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