{"id":23904,"date":"2024-12-24T21:46:55","date_gmt":"2024-12-24T13:46:55","guid":{"rendered":"https:\/\/wp-productionenv-bjg9h2g2bgg5b8aa.southeastasia-01.azurewebsites.net\/news\/europes-future-in-space-vega-cadence-to-increase-hyimpulses-hybrid-rocket\/"},"modified":"2024-12-24T21:46:55","modified_gmt":"2024-12-24T13:46:55","slug":"europes-future-in-space-vega-cadence-to-increase-hyimpulses-hybrid-rocket","status":"publish","type":"post","link":"https:\/\/starpath.global\/news\/europes-future-in-space-vega-cadence-to-increase-hyimpulses-hybrid-rocket\/","title":{"rendered":"Europe\u2019s future in space: Vega cadence to increase, HyImpulse\u2019s hybrid rocket"},"content":{"rendered":"<p>European companies in the space sector have been developing novel technology to find their unique place in the market, allowing them to thrive and innovate while stepping towards developing their orbital vehicles. Some are supported by the European Space Agency (ESA), such as HyImpulse, Isar Aerospace, and Orbex, while other independent private companies, such as PLD Space, are forging their ambitious paths to reusability.<\/p>\n<\/p>\n<p>Arianespace launched three European orbital missions in 2024 from the Guiana Space Centre in French Guiana. The first was the maiden launch of an Ariane 6 rocket in July, the successor to the Ariane 5 as Europe\u2019s premier heavy-lift vehicle. Ariane 6\u2019s first flight also marked the debut of the ELA-4 pad at the launch site. Two other missions placed Sentinel Earth observation satellites into Sun-synchronous orbits aboard Vega rockets, with the most recent of which being the return-to-flight of the troubled Vega C. Carrying the Sentinel-1C, which was originally intended to launch aboard a Soyuz vehicle, Vega C flew for the first time in almost two years.<\/p>\n<p><img fetchpriority=\"high\" decoding=\"async\" aria-describedby=\"caption-attachment-103888\" class=\"wp-image-103888 size-full\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Vega-launch-site-at-the-French-Guiana-Space-Center-Credit-ESA.jpg\" alt=\"\" width=\"1920\" height=\"852\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Vega-launch-site-at-the-French-Guiana-Space-Center-Credit-ESA.jpg 1920w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Vega-launch-site-at-the-French-Guiana-Space-Center-Credit-ESA-350x155.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Vega-launch-site-at-the-French-Guiana-Space-Center-Credit-ESA-630x280.jpg 630w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Vega-launch-site-at-the-French-Guiana-Space-Center-Credit-ESA-768x341.jpg 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Vega-launch-site-at-the-French-Guiana-Space-Center-Credit-ESA-1170x519.jpg 1170w\" sizes=\"(max-width: 1920px) 100vw, 1920px\"><\/p>\n<p id=\"caption-attachment-103888\" class=\"wp-caption-text\">Vega launch site at the French Guiana Space Center. (Credit: ESA)<\/p>\n<p>On Dec. 18, ESA signed multiple contracts with Avio, the manufacturer of the Vega rocket, to increase the annual number of flights of the Vega-C and to advance the development of its successor, the Vega-E. The former Ariane 5 integration building in French Guiana will be adapted for the Vega-C, enabling two mission campaigns to be prepared simultaneously, with one on the pad and the other in the upgraded assembly building. Four launches are planned for 2025, including the Biomass and Sentinel-1D missions, and another five in 2026.<\/p>\n<p>Avio took over Vega operations from Arianespace in late 2023 and will develop the next-generation Vega-E at the site, from the development of the rocket stages through to assembly and on-ground qualification testing. The Ariane 5 launch pad, fuelling, and support systems will be modified for the new vehicle. Vega-E stands slightly taller than Vega-C at 35 m with a 3.3 m diameter fairing. Using the P120C and Z40 motors developed for Vega C, it will have a liftoff thrust of 4,500 kN. The Zefiro 9 third stage and liquid-propelled Avum upper stages of the Vega-C will be replaced by a third, cryogenic MR10 upper stage, loaded with liquid methane and oxygen propellants just before launch. Vega-E\u2019s maiden launch is currently scheduled for 2027.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-103889\" class=\"wp-image-103889 size-full\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Render-of-the-Vega-E-Credit-ESA.jpg\" alt=\"\" width=\"1919\" height=\"1179\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Render-of-the-Vega-E-Credit-ESA.jpg 1919w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Render-of-the-Vega-E-Credit-ESA-350x215.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Render-of-the-Vega-E-Credit-ESA-570x350.jpg 570w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Render-of-the-Vega-E-Credit-ESA-180x110.jpg 180w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Render-of-the-Vega-E-Credit-ESA-768x472.jpg 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Render-of-the-Vega-E-Credit-ESA-1170x719.jpg 1170w\" sizes=\"(max-width: 1919px) 100vw, 1919px\"><\/p>\n<p id=\"caption-attachment-103889\" class=\"wp-caption-text\">Render of the Vega-E. (Credit: ESA)<\/p>\n<p>ESA recently awarded contract extensions to four companies as part of its Boost! program, which was designed to stimulate and support the development of space transportation services in member states. The program funded three companies in 2019 to reward industrial entrepreneurship and encourage competition within the private sector. November\u2019s \u20ac44.2 million funding extensions went to Isar Aerospace (\u20ac15 million), HyImpulse (\u20ac11.8 million), Rocket Factory Augsburg (\u20ac11.8 million), and UK-based Orbex (\u20ac5.6 million), who also began to receive funding from the program in 2021.<\/p>\n<p>German launch service company Isar Aerospace could potentially debut its Spectrum rocket in early 2025. This would also be the first orbital launch from the And\u00f8ya spaceport in Norway, which has supported over 300 suborbital missions for NASA since 1966. This site launched one of ten European suborbital launches in 2024, for the \u0141ukasiewicz Institute of Aviation. Most European suborbital flights have launched from the Esrange Space Center in Sweden, including the Red Kit, VSB-30, Dart, and the Improved Orion.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-103890\" class=\"wp-image-103890 size-full\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Render-of-Spectrum-rocket-on-the-pad-at-Andoya-Credit-Isar-Aerospace.jpg\" alt=\"\" width=\"1920\" height=\"1080\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Render-of-Spectrum-rocket-on-the-pad-at-Andoya-Credit-Isar-Aerospace.jpg 1920w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Render-of-Spectrum-rocket-on-the-pad-at-Andoya-Credit-Isar-Aerospace-350x197.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Render-of-Spectrum-rocket-on-the-pad-at-Andoya-Credit-Isar-Aerospace-622x350.jpg 622w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Render-of-Spectrum-rocket-on-the-pad-at-Andoya-Credit-Isar-Aerospace-768x432.jpg 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Render-of-Spectrum-rocket-on-the-pad-at-Andoya-Credit-Isar-Aerospace-1170x658.jpg 1170w\" sizes=\"(max-width: 1920px) 100vw, 1920px\"><\/p>\n<p id=\"caption-attachment-103890\" class=\"wp-caption-text\">Render of the Spectrum rocket on the pad at And\u00f8ya. (Credit: Isar Aerospace)<\/p>\n<p>German private aerospace company HyImpulse chose the Koonibba Test Range in Australia for its maiden flight. Headquartered in Neuenstadt am Kocher, it has been developing a series of products based around a hybrid rocket engine using a combination of paraffin-based fuel and liquid oxygen as propellant. The environmentally friendly technology is already being proven on the company\u2019s SR75 suborbital sounding rocket and will feed into the development of the forthcoming three-stage orbital SL1 using the same HyPLOX75 hybrid engine.<\/p>\n<p>     (adsbygoogle = window.adsbygoogle || []).push({});<\/p>\n<p>In mid-December, the company also announced an orbital transfer vehicle (OTV) called HyMove, which will use the same propellant technology. This OTV, also called a \u201cspace tug,\u201d will enable the company to deploy multiple satellites into different orbital planes from a single launch. The craft will support \u201clast mile\u201d payload delivery, precision orbital insertion, and hosted payload services. The company has partnered with leading nanosatellite mission provider Spacemanic to launch up to ten missions using HyMove from 2026 through 2036. The pair plan to capitalize on the expanding small satellite market in Europe, which is expected to grow to $30 billion by the decade\u2019s end. HyImpulse expects to wrap up ground testing of the space tug next year and begin flying commercial missions in 2029.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-103891\" class=\"wp-image-103891\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Render-of-the-HyMove-OTV-Credit-HyImpulse.jpg\" alt=\"\" width=\"819\" height=\"461\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Render-of-the-HyMove-OTV-Credit-HyImpulse.jpg 394w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Render-of-the-HyMove-OTV-Credit-HyImpulse-350x197.jpg 350w\" sizes=\"(max-width: 819px) 100vw, 819px\"><\/p>\n<p id=\"caption-attachment-103891\" class=\"wp-caption-text\">Render of the HyMove OTV. (Credit: HyImpulse)<\/p>\n<p>In May this year, the HyImpulse team launched its 12 m-long SR75 suborbital sounding rocket from the Koonibba Test Range. The rocket\u2019s name comes from the abbreviation \u201csounding rocket\u201d and the engine\u2019s 75 kN of thrust. It represented a significant change from the team\u2019s previous rockets.<\/p>\n<p>\u201cThe oxidizer change was the hard thing to do,\u201d Christian Schmierer, CEO of HyImpulse, told NSF. \u201cThat took roughly four years of intensive testing on the ground.\u201d<\/p>\n<p>The company was initially granted permission to launch from SaxaVord Spaceport in the Shetland Islands, with a 12-month window starting last December. While the Spaceport was yet to receive its launch license, the Civil Aviation Authority (CAA) granted permission to launch the SR75, considering the target altitude. Because the infrastructure was not yet in place, their first vehicle instead launched from Koonibba, reaching 50 km, and was recovered after a parachute descent. The team was on-site for three weeks, from the launch preparations and setting up the pad to the recovery of the rocket and packing away.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-103892\" class=\"wp-image-103892 size-full\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/SR75-lifts-off-from-Koonibba-Credit-HyImpulse.jpeg\" alt=\"\" width=\"2048\" height=\"1150\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/SR75-lifts-off-from-Koonibba-Credit-HyImpulse.jpeg 2048w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/SR75-lifts-off-from-Koonibba-Credit-HyImpulse-350x197.jpeg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/SR75-lifts-off-from-Koonibba-Credit-HyImpulse-623x350.jpeg 623w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/SR75-lifts-off-from-Koonibba-Credit-HyImpulse-768x431.jpeg 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/SR75-lifts-off-from-Koonibba-Credit-HyImpulse-1920x1078.jpeg 1920w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/SR75-lifts-off-from-Koonibba-Credit-HyImpulse-1170x657.jpeg 1170w\" sizes=\"(max-width: 2048px) 100vw, 2048px\"><\/p>\n<p id=\"caption-attachment-103892\" class=\"wp-caption-text\">SR75 lifts off from Koonibba Test Range in Australia. (Credit: HyImpulse)<\/p>\n<p>95% of the vehicle\u2019s technical development has been done in-house, and the company developed the automated fiber-winding technology and production capability to build its engines, composite tanks for both liquid oxygen and helium, avionics, and software. Constructed from a carbon-fiber-reinforced polymer, the company\u2019s Type 5 fully composite tank is both lightweight and strong, removing the need for a metal liner.<\/p>\n<p>Hybrid rocket engines<\/p>\n<p>HyImpulse is disruptive because of its hybrid rocket engine, which uses liquid oxygen and paraffin as liquefying fuel. The suborbital debut mission was dubbed \u201cLight This Candle\u201d as a nod to astronaut Alan Shepard\u2019s famous quote. The forthcoming SL-1 orbital rocket will benefit from utilizing a flight-proven engine design using this technology.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-103893\" class=\"wp-image-103893 size-full\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/HyImpulse-Production-of-the-SR75-Credit-HyImpulse-.png\" alt=\"\" width=\"1920\" height=\"1080\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/HyImpulse-Production-of-the-SR75-Credit-HyImpulse-.png 1920w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/HyImpulse-Production-of-the-SR75-Credit-HyImpulse--350x197.png 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/HyImpulse-Production-of-the-SR75-Credit-HyImpulse--622x350.png 622w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/HyImpulse-Production-of-the-SR75-Credit-HyImpulse--768x432.png 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/HyImpulse-Production-of-the-SR75-Credit-HyImpulse--1170x658.png 1170w\" sizes=\"(max-width: 1920px) 100vw, 1920px\"><\/p>\n<p id=\"caption-attachment-103893\" class=\"wp-caption-text\">Production of the SR75. (Credit: HyImpulse)<\/p>\n<p>\u201cThere are three major challenges with a hybrid rocket engine,\u201d Schmierer told NSF. \u201cThe first is the structural challenge of the large combustion chamber. There\u2019s 3,000 Kelvin inside, but you want to make it as light as possible, so you want to use composite fibers that will break at 80 degrees Celcius.\u201d<\/p>\n<p>If managing this wasn\u2019t enough of a challenge, the second difficulty is vaporizing the oxidizer. The student group used nitrous oxide, which is more or less already a monopropellant, so once ignited, it can keep the flame stable. \u201cLiquid oxygen is highly reactive,\u201d Schmierer notes, \u201cbut also cryogenic, so it cannot decide if it wants to make this flame burn really fast or to extinguish it if it\u2019s not refined.\u201d<\/p>\n<p>The third challenge is with the propellant fuel itself. \u201cThe classical hybrid rocket fuels, for example, Hydroxyl-terminated Polybutadiene (HTPB), is a chemical compound you\u2019ll also find in solid rocket motors as a binder. This burns faster than Hydrogen Peroxide (HTP) or other polymers, but it\u2019s still super slow. That has made it necessary in the past to have hybrid engines with complex geometries like a wagon wheel or a multiport, where there\u2019s a lot of holes in the fuel grain for the oxidizer to flow through. This increases the surface of the fuel and, therefore, the mass flow, which is dependent on the surface, but it has a big issue towards the end. The complex structure starts breaking apart as the fuel gets thinner, so you cannot fully burn [everything], and you have a huge amount of residual fuel.\u201d<\/p>\n<p>He notes that the solution is a circular port, limiting the design to one hole through which the oxidizer can be injected. The combustion then moves from inside to outside until it reaches the skin. However, with just one hole, there is no longer a large surface, so the fuel needs to burn faster to manage the regression rate.<\/p>\n<p>\u201cThis is where the liquefying technology comes in,\u201d Schmierer explains. \u201cThe paraffin fuel melts and forms a liquid layer on the surface, which forms waves and entrains droplets into the flow. This is the solution to the higher regression rate \u2013 by bringing droplets from the surface into the flame, you don\u2019t need to bring the flame to the surface. You reduce the necessary thermal heat exchange between the flame and the fuel by bringing the fuel to the flame.\u201d<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-103894\" class=\"wp-image-103894 size-full\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Ignition-as-the-SR75-takes-its-maiden-launch-Credit-HyImpulse.png\" alt=\"\" width=\"1920\" height=\"1080\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Ignition-as-the-SR75-takes-its-maiden-launch-Credit-HyImpulse.png 1920w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Ignition-as-the-SR75-takes-its-maiden-launch-Credit-HyImpulse-350x197.png 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Ignition-as-the-SR75-takes-its-maiden-launch-Credit-HyImpulse-622x350.png 622w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Ignition-as-the-SR75-takes-its-maiden-launch-Credit-HyImpulse-768x432.png 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Ignition-as-the-SR75-takes-its-maiden-launch-Credit-HyImpulse-1170x658.png 1170w\" sizes=\"(max-width: 1920px) 100vw, 1920px\"><\/p>\n<p id=\"caption-attachment-103894\" class=\"wp-caption-text\">SR75 ignites during its maiden launch. (Credit: HyImpulse)<\/p>\n<p>Paraffin is easily sourced, cheap to produce, and safely stored, but the choice is not without its challenges. In its pure form, it is very brittle and is sourced as a byproduct of the oil industry. HyImpulse has refined its recipe for the fuel with around five percent additives, fine-tuning the manufacturing process of mixing, melting, cooling down, and casting the solidified grain into blocks, which are then wrapped with composite fibers. \u201cIt\u2019s not an easy process \u2013 you can melt a few candles at home and try to pour it into a big shape and it will always break apart while solidifying because it shrinks extremely. As soon as you go to a three-meter paraffin with 60 cm diameter, then it starts to get really challenging.\u201d On the plus side, paraffin is chemically similar to kerosene and has the same specific impulse (ISP).<\/p>\n<p>HyImpulse views the suborbital SR75 as a progressive step towards scaling up its technology for the SL1 orbital rocket, nurturing and developing the team and the technology. \u201cOne use-case [for the SR75} is inaugural flights for multiple spaceports because they would like to have a rocket launch before they go orbital. We know that for microgravity research, there\u2019s a very limited market in Europe, and we could maybe launch two rockets a year in this market, so we never wanted to offer that service.\u201d<\/p>\n<p>\u201cThere is a lot of technology testing that is possible with this kind of rocket, such as testing material samples for supersonic and hypersonic flight, or payloads for space on a suborbital trajectory, for example, re-entry capsules. We have quite some customer interest and it could be as many as four to six launches per year.\u201d<\/p>\n<p>To support these future flights, an upgrade will increase the 30-second burn duration from the maiden flight and add active guidance to follow a predefined path with a fixed pitch. This is important for rockets of this size, which are wind-sensitive. The next flight will launch in Q1 of 2026 from Saxavord in the UK, which can be very windy while offering its customers more diverse mission profiles.<\/p>\n<\/p>\n<p><iframe title=\"HyImpulse: Hybrid Rocket Technology - NSF Live: Europe's Future in Space\" src=\"https:\/\/www.youtube.com\/embed\/Gsw-E5oJgbk?feature=oembed\" frameborder=\"0\" allow=\"accelerometer; autoplay; clipboard-write; encrypted-media; gyroscope; picture-in-picture; web-share\" referrerpolicy=\"strict-origin-when-cross-origin\" allowfullscreen=\"\" name=\"fitvid0\" data-gtm-yt-inspected-14=\"true\" data-gtm-yt-inspected-21=\"true\"><\/iframe><\/p>\n<p>As demonstrated by Firefly, responsive launches could be an emerging market that suits smaller rockets. However, the more significant challenge would be regulations and airspace impacts rather than the logistics of preparing hardware for launch. \u201cRight now, the time for a license in the UK is nine to 18 months, so the first step is to bring this down to nine months, then three, and of course, all these government institutions need to work together\u201d, Schmierer notes. He adds that regulators are unlikely to agree to less than the 72 hours Firefly currently works with because of the lead time to close the airspace. Paperwork aside, in the case of a paraffin engine, only the liquid oxidizer must be loaded for launch and is already available at most sites. HyImpulse could potentially store several launch-ready rockets at once, all already loaded with the paraffin propellant. This could even allow for the development of mobile launch sites.<\/p>\n<p>\u201cSimplicity translates into lower cost, not only in the manufacturing but in the whole process from testing, development, storage, and logistics. The biggest advantage for the customer is that we offer a small launcher that will be economically sustainable without government subsidies. It will be in the same order of magnitude as a Transporter mission, so while we will not reach $6,000 per kilogram \u2014 it may be two or three times as high in the beginning \u2014 we\u2019ll get closer to $8,000 or even $7,000.\u201d<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-103914\" class=\"wp-image-103914 size-full\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Orbex-Prime-seen-from-below-Credit-Orbex.jpg\" alt=\"\" width=\"1920\" height=\"1281\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Orbex-Prime-seen-from-below-Credit-Orbex.jpg 1920w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Orbex-Prime-seen-from-below-Credit-Orbex-350x234.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Orbex-Prime-seen-from-below-Credit-Orbex-525x350.jpg 525w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Orbex-Prime-seen-from-below-Credit-Orbex-768x512.jpg 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Orbex-Prime-seen-from-below-Credit-Orbex-1170x781.jpg 1170w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Orbex-Prime-seen-from-below-Credit-Orbex-585x390.jpg 585w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Orbex-Prime-seen-from-below-Credit-Orbex-263x175.jpg 263w\" sizes=\"(max-width: 1920px) 100vw, 1920px\"><\/p>\n<p id=\"caption-attachment-103914\" class=\"wp-caption-text\">Orbex Prime seen from below. (Credit: Orbex)<\/p>\n<p>SaxaVord Spaceport<\/p>\n<p>Five companies intend to launch from SaxaVord, which has a range license to launch 30 rockets annually. These include Orbex, which announced its plans to move flights to Shetland in early December after it decided to pause construction of its spaceport in Sutherland, Scotland, where the team first broke ground in May 2023. Using SaxaVord will enable Orbex to direct more of its funding to developing its medium-class launcher, Proxima.<\/p>\n<p>\u201cThe decision will help us reach the first launch in 2025 and provide SaxaVord with another customer to further strengthen its commercial proposition\u201d, said Orbex CEO Phil Chambers.<\/p>\n<p>This move came on the heels of the spaceport losing another customer, ABL Space Systems, which recently announced a pivot to missile defense programs in Nov. 2024. SaxaVord is also the choice for Edinburgh-based Skyrora and Rocket Factory Augsburg, whose RFA One rocket\u2019s first stage experienced an explosion during a static fire test of all nine Helix engines in August, causing \u201cminor repairs\u201d to be carried out on the launch stool.<\/p>\n<p>However, some customers see themselves outgrowing SaxaVord\u2019s capacity in their broader roadmap. \u201cIf you divide it by five and assume that, in five to ten years, all five are still there, you would have only six launches per company on average, which is not enough for us,\u201d Schmierer from HyImpulse says. \u201cEither some competitors drop out of the race, or we need a second launch site.\u201d For this reason, the company has already utilized a launch opportunity from Australia, which would give it a considerable advantage, as it is becoming geographically diversified and within reach of a growing customer base in the Asia-Pacific region.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-103896\" class=\"wp-image-103896 size-full\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/IMG_1682-1170x659-1.jpeg\" alt=\"\" width=\"1170\" height=\"659\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/IMG_1682-1170x659-1.jpeg 1170w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/IMG_1682-1170x659-1-350x197.jpeg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/IMG_1682-1170x659-1-621x350.jpeg 621w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/IMG_1682-1170x659-1-768x433.jpeg 768w\" sizes=\"(max-width: 1170px) 100vw, 1170px\"><\/p>\n<p id=\"caption-attachment-103896\" class=\"wp-caption-text\">RFA One static fires at SaxaVord in May 2024. (Credit: Rocket Factory Augsburg)<\/p>\n<p>\u201cOf course, French Guiana would be a nice launch site to reach orbits that are not highly inclined, but these are only around five percent of customer requests, so they are not a high priority right now. There is currently a regulation that a small amount, which could become bigger in the future, of European Union (EU) payloads have to be launched from EU territory. This could disqualify even the UK at this time.\u201d<\/p>\n<p>Future EU payloads that will stretch Europe\u2019s currently limited launch capacity will notably include the Infrastructure for Resilience, Interconnectivity, and Security by Satellite (IRIS\u00b2). By the end of the decade, this multi-orbital constellation will consist of 290 satellites in low and medium-Earth orbit. SpaceRISE, a consortium of European operators SES, Eutelsat,, and Hispasat, will operate the network.<\/p>\n<p>SL1 Orbital Launcher<\/p>\n<p>HyImpulse\u2019s 33 m long Small Launcher 1 (SL1) is planned to be capable of launching up to 600 kg on its first iteration. This is almost double that of Rocket Lab\u2019s Electron in height and payload capacity, with expectations to increase this capacity by at least a third in the future. With an optional kickstage for precise deployment into multiple orbital planes or inclinations, this three-stage vehicle suits rideshare and dedicated missions. The 2.2 m diameter design includes a new turbopump system for liquid oxygen.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-103897\" class=\"wp-image-103897 size-full\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Side-view-of-the-SL1-orbital-vehicle-Credit-HyImpulse.png\" alt=\"\" width=\"1920\" height=\"1080\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Side-view-of-the-SL1-orbital-vehicle-Credit-HyImpulse.png 1920w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Side-view-of-the-SL1-orbital-vehicle-Credit-HyImpulse-350x197.png 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Side-view-of-the-SL1-orbital-vehicle-Credit-HyImpulse-622x350.png 622w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Side-view-of-the-SL1-orbital-vehicle-Credit-HyImpulse-768x432.png 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Side-view-of-the-SL1-orbital-vehicle-Credit-HyImpulse-1170x658.png 1170w\" sizes=\"(max-width: 1920px) 100vw, 1920px\"><\/p>\n<p id=\"caption-attachment-103897\" class=\"wp-caption-text\">Side view of the SL1 orbital vehicle. (Credit: HyImpulse)<\/p>\n<p>\u201cIf you look at all the small launchers, I would claim that none of them are profitable, and you see this already in the U.S. \u2014 they either develop a larger vehicle or have integrated services such as launching their own satellites that they build for customers.\u201d Schmierer cites Rocket Lab with Neutron, Firefly with its MLV, Relativity skipping the Terran 1 to move to Terran R, and the incentives the European Space Agency is giving companies in this space with its funding of medium and heavy-lift rockets.<\/p>\n<p>\u201cLiquid rockets don\u2019t make sense on a small scale,\u201d he notes. \u201cIf you make something smaller, you reduce the material price a little, but the complexity of the vehicle assembly stays almost the same. If you reduce the payload by 90%, you will never reduce the price by [the same proportion].\u201d<\/p>\n<p>\u201cTo compare HyImpulse\u2019s hybrid engine with more traditional liquid engines, we need to compare the hybrid rocket casing with the thrust chamber of a liquid motor,\u201d Schmierer explains. The company expects to reduce the cost of a casing from the current \u20ac40,000 to half or a quarter of this cost over time. In contrast, a liquid thrust chamber will cost between \u20ac50,000 to \u20ac100,000, even with modern manufacturing technologies. The SL1 will use four of these casings in its first stage \u2014 four pumps will each feed two hybrid thrust chambers for the eight engines. By contrast, its competitors could use between 16 and 20 thrust chambers, depending on the number of engines. Even accounting for the economies of scale that come from higher production rates, the company sees this cost difference and the lower propellant cost as its competitive edge.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-103898\" class=\"wp-image-103898 size-full\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Engine-section-view-of-the-SL1-Credit-HyImpulse.png\" alt=\"\" width=\"1920\" height=\"1080\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Engine-section-view-of-the-SL1-Credit-HyImpulse.png 1920w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Engine-section-view-of-the-SL1-Credit-HyImpulse-350x197.png 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Engine-section-view-of-the-SL1-Credit-HyImpulse-622x350.png 622w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Engine-section-view-of-the-SL1-Credit-HyImpulse-768x432.png 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2024\/12\/Engine-section-view-of-the-SL1-Credit-HyImpulse-1170x658.png 1170w\" sizes=\"(max-width: 1920px) 100vw, 1920px\"><\/p>\n<p id=\"caption-attachment-103898\" class=\"wp-caption-text\">Render of the engine section of the SL1. (Credit: HyImpulse)<\/p>\n<p>The first two stages of the SL1 will use hybrid engines, while the third will use a liquid engine. This avoids complexities such as the high structural mass introduced by a long, thin hybrid motor on this upper stage. While the first SR75 flight was not actively controlled, the guidance and navigation control (GNC) algorithms have already been tested and are in the process of being refined, which helps the company step towards getting its orbital launch license in time.<\/p>\n<p>The engine section of the SL1 is where the rocket is visually distinct, with a square base. Initial designs were circular, with seven engines in a circle, but the change to feed two thrust chambers with one pump moved the count to an even number. \u201cWe played around with grouping eight engines and saw a few advantages,\u201d Schmierer told NSF. \u201cIt\u2019s symmetric \u2014 you could also arrange eight in a circle, but it\u2019s not symmetric, so here we basically have four propulsion units of the same configuration with the pumps together.\u201d He added that the outer dimensions have been checked to fit in a standard sea shipping container, whereas a circular design would not have fit.<\/p>\n<p>Reusability in Europe<\/p>\n<p>Spanish aerospace company PLD Space announced plans to upgrade its Miura 5 rocket with partial reusability in Nov. 2024, at the same time announcing a new family of rockets, Miura NEXT. This includes a range of medium to heavy-lift variants as part of an aggressive 10-year scale-up plan, including its production facilities. Following the successful launch of the company\u2019s Miura 1 pathfinder in late 2023, its focus has moved to the Muira 5, which will debut no earlier than late 2025. Five missions are initially planned yearly for its own SPARK program rather than paying customers. Starting with expendable launches, early missions will see the first stage returned under parachute. PLD is already targeting 2028 for the first stage of Miura 5 to return to land propulsively at a landing pad in the Guiana Space Center.<\/p>\n<\/p>\n<p><iframe title=\"PLD Space's Ambitious Plans for the Future  - NSF Live: Europe's Future in Space\" src=\"https:\/\/www.youtube.com\/embed\/2yltA7w9NfM?feature=oembed\" frameborder=\"0\" allow=\"accelerometer; autoplay; clipboard-write; encrypted-media; gyroscope; picture-in-picture; web-share\" referrerpolicy=\"strict-origin-when-cross-origin\" allowfullscreen=\"\" name=\"fitvid1\" data-gtm-yt-inspected-14=\"true\" data-gtm-yt-inspected-21=\"true\"><\/iframe><\/p>\n","protected":false},"excerpt":{"rendered":"<p>European companies in the space sector have been developing novel technology to find their unique place in the market, allowing them to thrive and innovate while stepping towards developing their orbital vehicles. Some are supported by the European Space Agency (ESA), such as HyImpulse, Isar Aerospace, and Orbex, while other independent private companies, such as [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"","ping_status":"","sticky":false,"template":"","format":"standard","meta":{"_acf_changed":false,"inline_featured_image":false,"footnotes":"","_links_to":"","_links_to_target":""},"categories":[2],"tags":[6748,8062,8168,1616,7463,8202,8203,916,8204],"class_list":["post-23904","post","type-post","status-publish","format-standard","hentry","category-news","tag-guiana-space-centre","tag-hybrid","tag-hyimpulse","tag-orbex","tag-saxavord","tag-sl1","tag-sr75","tag-vega-c","tag-vega-e"],"acf":[],"_links":{"self":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/23904"}],"collection":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/comments?post=23904"}],"version-history":[{"count":0,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/23904\/revisions"}],"wp:attachment":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media?parent=23904"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/categories?post=23904"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/tags?post=23904"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}