S5.4

Last updated
S5.4
Vostok spacecraft replica.jpg
Vostok spacecraft replica at the Technik Museum Speyer, Germany. The lower conical section was the service module with the S5.4/TDU-1 engine.
Country of origin USSR
Date1959-1961
First flight1959
Designer OKB-2, A.M. Isaev
ApplicationSpacecraft breaking engine
Successor S5.35
StatusRetired
Liquid-fuel engine
Propellant AK20F / TG-02
Mixture ratio3.07
Cycle Gas Generator
Configuration
Chamber1 main + 4 vernier
Performance
Thrust, vacuum15.83 kilonewtons (3,560 lbf)
Chamber pressure 5.6 megapascals (810 psi)
Specific impulse, vacuum266 seconds
Burn time45 seconds
Propellant capacity250 kilograms (550 lb)
Dimensions
Length1.13 metres (44 in)
Diameter0.95 metres (37 in)
Dry weight98 kilograms (216 lb)
Used in
Vostok, Voskhod and Zenit
References
References [1] [2] [3]

The S5.4 (AKA TDU-1, GRAU Index 8D66), was a Russian liquid rocket engine burning TG-02 and AK20F in the gas generator cycle. It was originally used as the braking (deorbit) engine of the Vostok, Voskhod, and Zenit spacecraft, which later switched to solid engines.[ citation needed ]

The engine produced 15.83 kilonewtons (3,560 lbf) of thrust with a specific impulse of 266 seconds in vacuum, and burned for 45 seconds, enough for the deorbit. It had a main fixed combustion chamber and four small verniers to supply vector control. It was housed in the service module and had two toroidal tanks for pressurization. [4] [5] [6]

It was designed by OKB-2, the Design Bureau led by Aleksei Isaev, for the Vostok program. The braking engine for the first manned spacecraft was a difficult task that no design bureau wanted to take.[ citation needed ] It was considered critical, as a failure would have left a cosmonaut stranded in space. A solid engine was considered, but the ballistic experts predicted a 500-kilometer (270-nautical-mile) landing error, versus a tenth of that for a liquid engine. It took the coordinated efforts of Boris Chertok and Sergei Korolev to convince Isaev to accept the task. [7]

Related Research Articles

<i>Buran</i> programme Soviet research project on spaceplanes

The Buran program, also known as the "VKK Space Orbiter programme", was a Soviet and later Russian reusable spacecraft project that began in 1974 at the Central Aerohydrodynamic Institute in Moscow and was formally suspended in 1993. In addition to being the designation for the whole Soviet/Russian reusable spacecraft project, Buran was also the name given to Orbiter K1, which completed one uncrewed spaceflight in 1988 and was the only Soviet reusable spacecraft to be launched into space. The Buran-class orbiters used the expendable Energia rocket as a launch vehicle. Unlike the Space Shuttle, Buran had a capability of flying uncrewed missions, as well as performing fully automated landings.

Soyuz (spacecraft) Series of spacecraft designed for the Soviet space programme

Soyuz is a series of spacecraft which has been in service since the 1960s, having made more than 140 flights. It was designed for the Soviet space program by the Korolev Design Bureau. The Soyuz succeeded the Voskhod spacecraft and was originally built as part of the Soviet crewed lunar programs. It is launched on a Soyuz rocket from the Baikonur Cosmodrome in Kazakhstan. Between the 2011 retirement of the Space Shuttle and the 2020 demo flight of SpaceX Crew Dragon, the Soyuz served as the only means to ferry crew to or from the International Space Station, for which it remains heavily used. Although China did launch crewed Shenzhou flights during this time, none of them docked with the ISS.

Voskhod 1 1964 Soviet spaceflight

Voskhod 1 was the seventh crewed Soviet space flight. Flown by cosmonauts Vladimir Komarov, Konstantin Feoktistov, and Boris Yegorov, it launched 12 October 1964, and returned on the 13th. Voskhod 1 was the first human spaceflight to carry more than one crewman into orbit, the first flight without the use of spacesuits, and the first to carry either an engineer or a physician into outer space. It also set a crewed spacecraft altitude record of 336 km (209 mi).

Voskhod 2 Soviet manned spaceflight; worlds first space walk

Voskhod 2 was a Soviet crewed space mission in March 1965. The Vostok-based Voskhod 3KD spacecraft with two crew members on board, Pavel Belyayev and Alexei Leonov, was equipped with an inflatable airlock. It established another milestone in space exploration when Alexei Leonov became the first person to leave the spacecraft in a specialized spacesuit to conduct a 12-minute spacewalk.

Solid rocket booster Solid propellant motor used to augment the thrust of a rocket

A solid rocket booster (SRB) is a large solid propellant motor used to provide thrust in spacecraft launches from initial launch through the first ascent. Many launch vehicles, including the Ariane 5, Atlas V, and space shuttle, have used SRBs to give launch vehicles much of the thrust required to place the vehicle into orbit. The space shuttle used two space shuttle SRBs, which were the largest solid propellant motors ever built and the first designed for recovery and reuse. The propellant for each solid rocket motor on the space shuttle weighed approximately 500,000 kilograms.

Soviet space program Space exploration program conducted by the Soviet Union from the 1950s to 1991.

The Soviet space program was the national space program of the former Union of Soviet Socialist Republics (USSR), active from 1955 until the dissolution of the Soviet Union in 1991.

Korabl-Sputnik 3 or Vostok-1K No.3, also known as Sputnik 6 in the West, was a Soviet spacecraft which was launched in 1960. It was a test flight of the Vostok spacecraft, carrying two dogs; Pcholka and Mushka, as well as a television camera and scientific instruments.

Space capsule Type of spacecraft

A space capsule is an often-crewed spacecraft that uses a blunt-body reentry capsule to reenter the Earth's atmosphere without wings. Capsules are distinguished from other satellites primarily by the ability to survive reentry and return a payload to the Earth's surface from orbit. Capsule-based crewed spacecraft such as Soyuz or Orion are often supported by a service or adapter module, and sometimes augmented with an extra module for extended space operations. Capsules make up the majority of crewed spacecraft designs, although one crewed spaceplane, the Space Shuttle, has flown in orbit.

Launch escape system System to get the crew to safety if a rocket launch fails

A launch escape system (LES) or launch abort system (LAS) is a crew-safety system connected to a space capsule that can be used to quickly separate the capsule from its launch vehicle in case of an emergency requiring the abort of the launch, such as an impending explosion. The LES is typically controlled by a combination of automatic rocket failure detection, and a manual activation for the crew commander's use. The LES may be used while the launch vehicle is still on the launch pad, or during its ascent. Such systems are usually of two types:

Bereznyak-Isayev BI-1 Type of aircraft

The Bereznyak-Isayev BI-1 was a Soviet short-range rocket powered interceptor developed during the Second World War.

Spacecraft electric propulsion Type of space propulsion

Spacecraft electric propulsion is a type of spacecraft propulsion technique that uses electrostatic or electromagnetic fields to accelerate mass to high speed and thus generate thrust to modify the velocity of a spacecraft in orbit. The propulsion system is controlled by power electronics.

Orion abort modes Launch abort modes used by the Orion spacecraft

The Orion Multi-Purpose Crew Vehicle is a class of partially reusable spacecraft used in NASA's human spaceflight programs. Consisting two components – a Crew Module (CM) manufactured by Lockheed Martin, and a European Service Module (ESM) manufactured by Airbus Defence and Space – the spacecraft are designed to support crewed exploration beyond low Earth orbit. Orion is equipped with solar power, an automated docking system, and glass cockpit interfaces modeled after those used in the Boeing 787 Dreamliner, and can support a crew of six up to 21 days undocked and up to six months docked. A single AJ10 engine provides the spacecraft's primary propulsion, while eight R-4D-11 engines and six pods of custom reaction control system engines developed by Airbus provide the spacecraft's secondary propulsion. Although compatible with other launch vehicles, Orion is primarily designed to launch atop a Space Launch System (SLS) rocket, with a tower launch escape system.

RD-107 Russian rocket engine

The RD-107 and its sibling, the RD-108, are a type of rocket engine initially used to launch R-7 Semyorka missiles. RD-107 engines were later used on space launch vehicles based on the R-7. As of 2021, very similar RD-107A and RD-108A engines are used to launch the Soyuz-2.1a, and Soyuz-2.1b, which are in active service.

RD-0109 Rocket engine

The RD-0109 is a rocket engine burning liquid oxygen and kerosene in a gas generator combustion cycle. It has single nozzle and is an evolution of the RD-0105. It was the engine used on the Vostok Block-E that launched Yuri Gagarin to orbit.

The KTDU-35 was a Soviet spacecraft propulsion system composed of two liquid rocket engines, the primary, S5.60 (SKD) and the secondary S5.35 (DKD), fed from the same propellant tanks. Both engines burn UDMH and AK27I in the gas generator cycle. It was designed by OKB-2, the famous Isaev Design Bureau, for the original Soyuz programme.

The S5.80 is a liquid pressure-fed rocket engine burning N2O4/UDMH with an O/F of 1.85. It is used for crew-rated spacecraft propulsion applications. It is currently used in the Soyuz-TMA-M spacecraft propulsion module KTDU-80, and its sibling, the S5.79 rocket engine, is still used as the main propulsion of the Zvezda ISS module. The S5.80 generates 2.95 kN (660 lbf) of thrust with a chamber pressure of 0.88 MPa (128 psi) and a nozzle expansion of 153.8 that enables it to achieve a specific impulse of 302 s (2.96 km/s). It is rated for 30 starts with a total firing time of 890 seconds. The engine, without the pressurization system or propellant tanks, weighs 310 kg (680 lb) and is an integrated unit that is 1.2 m (47 in) long with a diameter of 2.1 m (83 in).

A.M. Isayev Chemical Engineering Design Bureau

The A.M. Isayev Chemical Engineering Design Bureau, also known as KB KhimMash or just KBKhM, is a Russian rocket engine design and manufacturing company. It is located in the city of Korolyov. It started as the OKB-2 division of the NII-88 research institute, where A.Isaev directed the development of liquid rocket engines for ballistic missile submarines.

Leonid Voskresensky Soviet rocket engineer

Leonid Alexandrovich Voskresensky was a Soviet rocket engineer and long-time associate of Chief Designer Sergei Korolev. He served as launch director for Sputnik and for the first manned space flight, Vostok 1. The lunar crater Voskresenskiy is named in his honor.

Soviet rocketry Soviet rocketry (1921 to 1991)

Soviet rocketry commenced in 1921 with development of Solid-fuel rockets, which resulted in the development of the Katyusha rocket launcher. Rocket scientists and engineers, particularly Valentin Glushko and Sergei Korolev, contributed to the development of Liquid-fuel rockets, which were first used for fighter aircraft and later for ballistic missiles, and space exploration. Progress was greatly augmented by the reverse engineering of Nazi German technology captured by westward-moving troops during the final days of World War II and the immediate period following, though after 1947 their influence was marginal. Developments continued in the 1950s with a variety of ICBMs and resulted in the launch of Sputnik 1 in 1957, the first artificial Earth satellite ever launched.

References

  1. Brügge, Norbert. "Spacecraft-propulsion blocks (KDU) from Isayev's design bureau (now Khimmash)". B14643.de. Archived from the original on 2015-06-02. Retrieved 2015-06-02.
  2. "S5.4". Encyclopedia Astronautica. Archived from the original on August 27, 2002. Retrieved 2015-07-25.
  3. Pillet, Nicolas. "Le vaisseau Vostok" [The Vostk spacecraft] (in French). Kosmonavtika.com. Retrieved 2015-07-25.
  4. Zak, Anatoly. "Origin of the Vostok spacecraft". RussianSpaceWeb. Retrieved 2015-07-25.
  5. LePage, Andrew J. "Vostok: an aerospace classic". The Space Review . Retrieved 2015-07-15.
  6. Turner, Martin J. L. (2008). "Section 9.2 Crewed launchers and re-entry vehicles". Rocket and Spacecraft Propulsion: Principles, Practice and New Developments. Springer Science & Business Media. p. 314. ISBN   978-3540692034 . Retrieved 2015-07-15.
  7. Chertok, Boris (May 2009). "Chapter 2 Preparation for Piloted Flights". Rockets and People Vol. 3 Hot Days of the Cold War (PDF). Vol. 3 (NASA SP-2006-4110). NASA. p. 26. ISBN   978-0-16-081733-5 . Retrieved 2015-07-15.