Flame deflector

Last updated
The main flame deflector in the flame trench at Launch Complex 39B at NASA's Kennedy Space Center in Florida. It deflects the plume exhaust from NASA's Space Launch System rocket during launch. It features a new "steel plated" design and incorporates water pipes for sound suppression. Flame Deflector Complete at Launch Complex 39B (KSC-20180516-PH KLS01 0007).jpg
The main flame deflector in the flame trench at Launch Complex 39B at NASA's Kennedy Space Center in Florida. It deflects the plume exhaust from NASA's Space Launch System rocket during launch. It features a new "steel plated" design and incorporates water pipes for sound suppression.

A flame deflector, flame diverter or flame trench is a structure or device designed to redirect or disperse the flame, heat, and exhaust gases produced by rocket engines or other propulsion systems. [2] The amount of thrust generated by a rocket launch, along with the sound it produces during liftoff, can damage the launchpad and service structure, as well as the launch vehicle. [3] The primary goal of the diverter is to prevent the flame from causing damage to equipment, infrastructure, or the surrounding environment. Flame diverters can be found at rocket launch sites and test stands where large volumes of exhaust gases are expelled during engine testing or vehicle launch.

Contents

Design and operation

The diverter typically comprises a robust, heat-resistant structure that channels the force of the exhaust gases and flames in a specific direction, typically away from the rocket or equipment. This is essential to prevent the potentially destructive effects of the high-temperature gases and to reduce the acoustic impact of the ignition.

A flame trench can also be used in combination with a diverter to form a trench-deflector system. The flames from the rocket travel through openings in the launchpad onto a flame deflector situated in the flame trench, which runs underneath the launch structure and extends well beyond the launchpad itself. [3] To further reduce the acoustic effects a water sound suppression system may be also used.

Notable examples

Apollo program

During the Apollo program the need for a flame deflector was a determining factor in the design of the Kennedy Space Center Launch Complex 39. NASA designers chose a two-way, wedge-type metal flame deflector. It measured 13 meters in height and 15 meters in width, with a total weight of 317 tons. Since the water table was close to the surface of the ground, the designers wanted the bottom of the flame trench at ground level. The flame deflector and trench determined the height and width of the octagonal shaped launch pad. [2]

Space Shuttle program

The Shuttle flame trench-deflector system under a vehicle ready for launch. Stspad39aflamepit.jpg
The Shuttle flame trench-deflector system under a vehicle ready for launch.

During the Space Shuttle program NASA modified Launch Complex 39B at Kennedy Space Center. They installed a flame trench that was 150 meters long, 18 meters wide, and 13 meters deep. [3] It was built with concrete and refractory brick. The main flame deflector was situated inside the trench directly underneath the rocket boosters. The V-shaped steel structure was covered with a high-temperature concrete material. It separated the exhaust of the orbiter main engines and of the solid rocket boosters into two flame trenches. [4] [5] It was approximately 11.6 meters high, 17.5 meters wide, and 22 meters long. [3] The Shuttle flame trench-diverter system was refurbished for the SLS program. [4] [6]

Baikonur Cosmodrome

A Soyuz rocket erected into position at the launch padat the Baikonur Cosmodrome in Kazakhstan in 2009. The flame deflector and pit is visible below. Soyuz expedition 19 launch pad.jpg
A Soyuz rocket erected into position at the launch padat the Baikonur Cosmodrome in Kazakhstan in 2009. The flame deflector and pit is visible below.

The main launch pads at the Russian launch complex of Baikonur Cosmodrome use a flame pit to manage launch exhaust. The launch vehicles are transported by rail to the launch pad, where they are vertically erected over a large flame deflector pit. [7] A similar structure was built by the European Space Agency at its Guiana Space Centre. [7]

SpaceX Starship launch mount

During the first orbital test flight of SpaceX's Starship vehicle in April 2023, the launch mount of Starbase was substantially damaged due to the lack of a flame diverter system. [8] The 33 Raptor rocket engines dug a 25-foot-deep crater and scattered debris and dust over a wide area. [8] The company designed a new water deluge based flame diverter that protects the launch mount and vehicle by spraying large quantities of water from a piece of steel equipment under the rocket. [9] [8] In November of the same year, the new water deluge system successfully protected the launchpad during the second orbital flight test of Spaceship, avoiding the cloud of dust and debris that rose up during the first test. [10]

Related Research Articles

<span class="mw-page-title-main">Rocket</span> Vehicle propelled by a reaction gas engine

A rocket is a vehicle that uses jet propulsion to accelerate without using the surrounding air. A rocket engine produces thrust by reaction to exhaust expelled at high speed. Rocket engines work entirely from propellant carried within the vehicle; therefore a rocket can fly in the vacuum of space. Rockets work more efficiently in a vacuum and incur a loss of thrust due to the opposing pressure of the atmosphere.

<span class="mw-page-title-main">Launch pad</span> Facility from which rockets are launched

A launch pad is an above-ground facility from which a rocket-powered missile or space vehicle is vertically launched. The term launch pad can be used to describe just the central launch platform, or the entire complex. The entire complex will include a launch mount or launch platform to physically support the vehicle, a service structure with umbilicals, and the infrastructure required to provide propellants, cryogenic fluids, electrical power, communications, telemetry, rocket assembly, payload processing, storage facilities for propellants and gases, equipment, access roads, and drainage.

<span class="mw-page-title-main">Delta IV</span> Active expendable launch system in the Delta rocket family

Delta IV was a group of five expendable launch systems in the Delta rocket family introduced in the early 2000s. Originally designed by Boeing's Defense, Space and Security division for the Evolved Expendable Launch Vehicle (EELV) program, the Delta IV became a United Launch Alliance (ULA) product in 2006. The Delta IV was primarily a launch vehicle for United States Air Force (USAF) military payloads, but was also used to launch a number of United States government non-military payloads and a single commercial satellite.

<span class="mw-page-title-main">N1 (rocket)</span> Soviet super heavy-lift launch vehicle

The N1/L3 was a super heavy-lift launch vehicle intended to deliver payloads beyond low Earth orbit. The N1 was the Soviet counterpart to the US Saturn V and was intended to enable crewed travel to the Moon and beyond, with studies beginning as early as 1959. Its first stage, Block A, was the most powerful rocket stage ever flown for over 50 years, generating 45.4 MN of thrust. However, each of the four attempts to launch an N1 failed in flight, with the second attempt resulting in the vehicle crashing back onto its launch pad shortly after liftoff. Adverse characteristics of the large cluster of thirty engines and its complex fuel and oxidizer feeder systems were not revealed earlier in development because static test firings had not been conducted.

<span class="mw-page-title-main">Blue Origin</span> American aerospace company

Blue Origin, LLC is an American aerospace manufacturer, defense contractor, launch service provider and space technologies company headquartered in Kent, Washington, United States. The company makes rocket engines for United Launch Alliance (ULA) and manufactures their own rockets, spacecraft, satellites, and heavy-lift launch vehicles. The company is the second provider of lunar lander services for NASA's Artemis program and was awarded a $3.4 billion contract. The company has three rocket engines in production including the BE-3U, BE-3PM and BE-4. The company is working on a fourth rocket engine called the BE-7 which is still under development and when completed may be used on planetary bodies other than Earth.

<span class="mw-page-title-main">Kennedy Space Center Launch Complex 39A</span> Historic launch pad operated by NASA and SpaceX

Launch Complex 39A (LC-39A) is the first of Launch Complex 39's three launch pads, located at NASA's Kennedy Space Center in Merritt Island, Florida. The pad, along with Launch Complex 39B, was first designed to accommodate the Saturn V launch vehicle. Typically used to launch NASA's crewed spaceflight missions since the late 1960s, the pad was leased by SpaceX and has been modified to support their launch vehicles.

<span class="mw-page-title-main">Crawler-transporter</span> NASA rocket transport vehicle

The crawler-transporters, formally known as the Missile Crawler Transporter Facilities, are a pair of tracked vehicles used to transport spacecraft from NASA's Vehicle Assembly Building (VAB) along the Crawlerway to Launch Complex 39. They were originally used to transport the Saturn IB and Saturn V rockets during the Apollo, Skylab and Apollo–Soyuz programs. They were then used to transport Space Shuttles from 1981 to 2011. The crawler-transporters carry vehicles on the mobile launcher platforms used by NASA, and after each launch return to the pad to take the platform back to the VAB.

<span class="mw-page-title-main">Kennedy Space Center Launch Complex 39</span> Historic Apollo Moonport

Launch Complex 39 (LC-39) is a rocket launch site at the John F. Kennedy Space Center on Merritt Island in Florida, United States. The site and its collection of facilities were originally built as the Apollo program's "Moonport" and later modified for the Space Shuttle program.

<span class="mw-page-title-main">Mobile launcher platform</span> Structure used to support large rockets

A mobile launcher platform (MLP), also known as mobile launch platform, is a structure used to support a large multistage space vehicle which is assembled (stacked) vertically in an integration facility and then transported by a crawler-transporter (CT) to a launch pad. This becomes the support structure for launch.

<span class="mw-page-title-main">Rocket engine test facility</span> Location where rocket engines may be tested on the ground, under controlled conditions

A rocket engine test facility is a location where rocket engines may be tested on the ground, under controlled conditions. A ground test program is generally required before the engine is certified for flight. Ground testing is very inexpensive in comparison to the cost of risking an entire mission or the lives of a flight crew.

<span class="mw-page-title-main">Kennedy Space Center Launch Complex 39B</span> Historic launch pad operated by NASA

Launch Complex 39B (LC-39B) is the second of Launch Complex 39's three launch pads, located at NASA's Kennedy Space Center in Merritt Island, Florida. The pad, along with Launch Complex 39A, was first designed for the Saturn V launch vehicle, which at the time was the United States' most powerful rocket. Typically used to launch NASA's crewed spaceflight missions since the late 1960s, the pad is currently configured for use by the agency's Space Launch System rocket, a Shuttle-derived launch vehicle which is currently used in the Artemis program and subsequent Moon to Mars campaigns. The pad had also been leased by NASA to aerospace company Northrop Grumman, for use as a launch site for their Shuttle-derived OmegA launch vehicle, for National Security Space Launch flights and commercial launches, before the OmegA program was cancelled.

Fondu Fyre, sometimes called Fondue Fyre, is a refractory concrete developed for specialist application. Fondu Fyre is a heat and erosion resistant concrete developed during the Apollo space program. It was developed to withstand the supersonic plume of a rocket engine during launch and hot-fire tests.

<span class="mw-page-title-main">Mid-Atlantic Regional Spaceport Launch Pad 0</span> Rocket launch complex on Wallops Island, Virginia, U.S.

Launch Pad 0 (LP-0), also known as Launch Complex 0 (LC-0), or Launch Area 0 (LA-0), is a launch complex at the Mid-Atlantic Regional Spaceport (MARS) on Wallops Island, Virginia, in the United States. MARS is located adjacent to NASA's Wallops Flight Facility (WFF), which ran the launch complex until 2003. WFF continues to provide various support services to MARS launches under contract with the Commonwealth of Virginia.

<span class="mw-page-title-main">SpaceX facilities</span> Launch facilities used by SpaceX

As of 2023, SpaceX operates four launch facilities: Cape Canaveral Space Launch Complex 40 (SLC-40), Vandenberg Space Force Base Space Launch Complex 4E (SLC-4E), Kennedy Space Center Launch Complex 39A (LC-39A), and Brownsville South Texas Launch Site (Starbase). Space Launch Complex 40 was damaged in the AMOS-6 accident in September 2016 and repair work was completed by December 2017. SpaceX believes that they can optimize their launch operations, and reduce launch costs, by dividing their launch missions amongst these four launch facilities: LC-39A for NASA launches, SLC-40 for United States Space Force national security launches, SLC-4E for polar launches, and South Texas Launch Site for commercial launches.

Sites for launching large rockets are often equipped with a sound suppression system to absorb or deflect acoustic energy generated during a rocket launch. As engine exhaust gasses exceed the speed of sound, they collide with the ambient air and shockwaves are created, with noise levels approaching 200 db. This energy can be reflected by the launch platform and pad surfaces, and could potentially cause damage to the launch vehicle, payload, and crew. For instance, the maximum admissible overall sound power level (OASPL) for payload integrity is approximately 145 db. Sound is dissipated by huge volumes of water distributed across the launch pad and launch platform during liftoff.

<span class="mw-page-title-main">Exploration Ground Systems</span> NASA program for launch vehicle support

NASA's Exploration Ground Systems (EGS) Program is one of three programs based at NASA's Kennedy Space Center in Florida. EGS was established to develop and operate the systems and facilities necessary to process and launch rockets and spacecraft during assembly, transport and launch. EGS is preparing the infrastructure to support NASA's Space Launch System (SLS) rocket and its payloads, such as the Orion spacecraft for Artemis I. Artemis I is the first to launch in a series of increasingly complex missions that will enable human exploration to the Moon and Mars.

<span class="mw-page-title-main">SpaceX Starship</span> Super heavy-lift reusable launch vehicle

Starship is a two-stage super heavy lift launch vehicle and spacecraft under development by SpaceX. It is the heaviest, tallest and most powerful space launch vehicle to have flown. Starship is intended to be fully reusable, which means both stages will be recovered after a mission and reused.

<span class="mw-page-title-main">AgniKul Cosmos</span> Indian aerospace company

AgniKul Cosmos Private Limited is an Indian aerospace manufacturer based in National Center for Combustion R&D (NCRD) of IIT Madras, Chennai. The start up aims to develop and launch its own small-lift launch vehicle such as the Agnibaan, capable of placing 100 kg (220 lb) payload into a 700 km (430 mi) orbit. The first commercial launch was expected in 2022. However, no launch happened in that year.

<span class="mw-page-title-main">SpaceX Starship first integrated flight test</span> First integrated test launch of SpaceX Starship

On April 20, 2023, SpaceX performed the first integrated near-orbital flight of its Starship rocket. The prototype vehicle was destroyed less than four minutes after lifting off from the SpaceX Starbase in Boca Chica, Texas. The vehicle became the most powerful rocket ever flown, breaking the half-century-old record held by the Soviet Union's N1 rocket.

<span class="mw-page-title-main">SpaceX Starship second integrated flight test</span> Second launch of SpaceX Starship

On November 18, 2023, SpaceX performed the second integrated near-orbital flight of its Starship rocket. The Starship successfully lifted off under the power of all 33 Raptor engines on the Super Heavy booster and made it through stage separation. Then, the booster had multiple engine failures and exploded, while the Starship continued to fly for over 8 minutes, reaching an altitude of 148 km (92 mi), above the boundary of space, before also disintegrating. The Federal Aviation Administration issued a statement confirming that an anomaly had occurred and that there are no reports of public property damage or injuries. SpaceX described the test as a success.

References

  1. Herridge, Linda (2018-05-29). "Launch Pad 39B Flame Trench Nears Completion". NASA. Retrieved 2023-09-01.
  2. 1 2 "Moonport, CH11-7". www.hq.nasa.gov. Retrieved 2023-09-01.
  3. 1 2 3 4 Wessels, Wessel (2022-10-26). "The Purpose Of A Flame Trench At A Rocket Launch Site". Headed For Space. Retrieved 2023-09-01.
  4. 1 2 "Deflecting the flames of a monster rocket". The Planetary Society. Retrieved 2023-09-01.
  5. Warnock, Lynda. "NASA - Flame Trench-Deflector System". www.nasa.gov. Retrieved 2023-09-01.
  6. Bergin, Chris (2016-05-08). "Renewing the famous Flame Trench, one brick at a time". NASASpaceFlight.com. Retrieved 2023-09-01.
  7. 1 2 "Launcher". www.esa.int. Retrieved 2023-09-02.
  8. 1 2 3 "SpaceX Tests Starship Water Deluge System That It Should've Built in the First Place". Gizmodo. 2023-07-18. Retrieved 2023-09-01.
  9. Kolodny, Lora (2023-07-28). "SpaceX hasn't obtained environmental permits for 'flame deflector' system it's testing in Texas". CNBC. Retrieved 2023-09-01.
  10. Chang, Kenneth (2023-11-18). "SpaceX Makes Progress in 2nd Launch of Giant Moon and Mars Rocket". The New York Times. ISSN   0362-4331 . Retrieved 2023-11-20.