Firefly Aerospace

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Firefly Aerospace, Inc.
legal form Incorporated
founding 2014/2017
Seat Cedar Park , Texas ,
United States
management Thomas Markusic,
Max Poljakow,
Mark Watt (directors)
Number of employees approx. 320 (end of 2018)
Branch Space travel
Website firefly.com
Figure: Alpha (2018)
Alpha Profile High Res Vertical.png

Firefly Aerospace is a US - Ukrainian aerospace company. Firefly is developing two launch vehicles : the Alpha (also Firefly α ) for payloads up to 1  t and the Beta ( Firefly β ) for payloads up to 8 t. A first flight of the Alpha is planned for 2020.

Firefly Aerospace means " Firefly -Aerospace". A stylized firefly also forms the company logo.

history

In January 2014 the engineer Thomas Markusic founded the company Firefly Space Systems . It was one of many small rocket manufacturers that emerged in anticipation of a boom in the small satellite market . Markusic had previously worked for NASA , SpaceX , Blue Origin and Virgin Galactic . With Firefly he started the development of the two-stage rocket Alpha . It should use methane as fuel and be able to transport 400 kg payload. As a special innovation, an engine with twelve combustion chambers in an aerospike arrangement was planned for the first rocket stage . Like SpaceX, Firefly Space Systems was initially based in Hawthorne , California , but after nine months it relocated to Cedar Park , a suburb of the Texas capital Austin .

In the founding year, a legal dispute with Virgin Galactic overshadowed the course of business. Virgin accused Markusic, among other things, of stealing trade secrets and materials and using them for the development of the Alpha. He has since destroyed the evidence for this. As Firefly engineers began testing the new aerospike engine, the dispute with Virgin escalated. In August 2016, an arbitration tribunal upheld the accusation of destruction of evidence. Shortly afterwards, an important investor withdrew. Firefly got into a financial crisis and had to cease operations. As a result, the only start order issued by NASA was lost.

The assets of the insolvent rocket manufacturer were bought by the Ukrainian investor Max Polyakov in 2017. Polyakov formed from the new Firefly Aerospace, Inc . The company's operational headquarters remained in Cedar Park; In 2018 there was also a development office in Dnipro , the center of the Ukrainian space industry. Soon more people were working in the Ukrainian branch than in the USA.

Under Polyakov's control, the planned missile was considerably enlarged; In addition, a conventional engine design was also chosen for the first stage. First tests of the complete engine took place in March 2019. The development of the second stage was already further advanced at this point; it successfully completed a five-minute test run in April.

In October 2019, Firefly announced that it would collaborate with Aerojet Rocketdyne on engine development .

Locations and facilities

Ukrainian President Petro Poroshenko (2nd from right) at the opening of the Firefly branch in Dnipro

Firefly's development work is split between the two facilities in Cedar Park and Dnipro. The company also operates a production and test center about 50 kilometers north of the Texas headquarters.

Two existing launch ramps on the US east and west coast are to be taken over and prepared for the rocket launches . Highly inclined orbits are to be operated from Space Launch Complex 2W at Vandenberg Air Force Base in California. This launch site was used for the Delta II until 2018 . Space Launch Complex 20 on Cape Canaveral Air Force Station in Florida, which was closed in 2000, is intended for smaller orbit inclines . In the vicinity of the SLC-20 - in the "Exploration Park" industrial park at the Kennedy Space Center - a factory for series production of the Alpha is also to be built. [date] at this site are among others already factories for large rocket New Glenn and OneWeb - communications satellites .

Firefly Alpha

use

Even in its enlarged form, the Alpha is a vehicle for launching small satellites . The manufacturer mentions 1000 kg as the payload capacity for low earth orbits (LEO). Up to 630 kg should be able to be transported in a 500 km high sun-synchronous orbit (SSE). With an additionally planned kick stage, it should also be possible to transport 600 kg into geostationary orbits and 500 kg to the moon. For a later version of the rocket, more than 800 kg SSO payload capacity is targeted.

Firefly concluded various framework agreements to market the rocket. Among other things, agreements exist with the British satellite manufacturer Surrey Satellite Technology (SSTL), the US launch agent Spaceflight Industries , the Italian space service provider D-Orbit and the multinational aerospace company Airbus Defense and Space . The price per start should be around 15 million US dollars.

The first flight of the Alpha was initially planned for 2016. As usual in the space industry, this date has been postponed several times. In June 2019, a first flight was announced for 2020.

Thomas Markusic named the PSLV rocket from the Indian space agency ISRO as the most important competitor product . Competition is also emerging directly in the USA with the RS1 from ABL Space Systems and the Terran 1 from Relativity Space .

technical structure

Functional diagram of all Firefly engines (simplified)

The Alpha is designed as a two-stage rocket. An optional third stage, which would be transported as a kick stage within the payload section, has been announced since November 2018; At least until May 2019, however, no development schedule has yet been announced.

The outer shell and tanks of the first and second rocket stages, as well as the payload fairing, are made of carbon fiber-reinforced plastic . Thanks to this lightweight construction , the almost 30-meter-high rocket weighs only 3.8 tons. The maximum take-off mass including fuel and payload is 54 tons.

All Alpha engines are powered by rocket kerosene (RP-1) and liquid oxygen . They are regeneratively cooled and work according to the tap-off cycle ; that is, the nozzle wall is cooled with the fuel passed through, while the fuel and oxygen pumps are driven by a turbine , which in turn is operated with hot gas drawn off from the combustion chamber . In the first stage there are four such motors with the designation Reaver 1 , in the second one called Lightning 1 ("Blitz 1"). Firefly gives the total thrust in the vacuum as 736  kN for the first and 70 kN for the second stage. However, the first stage would not be used in a vacuum, but within the atmosphere, where the engines generate less thrust.

Further technical data are listed in the data table .

Starts

In July 2019, Firefly announced that the Alpha had launch contracts worth $ 560 million. At a price of $ 15 million each, this equates to around 35–40 starts. With the exception of a test satellite for SSTL, however, no commercial customers or payloads were named. On its first flight, Firefly transports payloads for academic purposes free of charge.

The following planned launches are known individually (as of April 23, 2020):

Date ( UTC ) Launch site Customer / payload Type / purpose of the payload Payload
(kg) 2
Orbit 3
2020 VAFB SLC-2W Spinnaker 3
NPS-Centix-Orbital 1
TIS Cubekit
BSS1
Hiapo
Magneto
FossaCon-1
Cresst Dream Comet
Firefly Capsule 1
Awning
communication experiment
flight data acquisition
technology testing
research
experiments
eight Pocketqubes
technology testing
time capsule
LEO
2020 VAFB SLC-2W United KingdomUnited Kingdom Carbonite-4
More Payloads?
Experimental satellite
 
LEO
Mid-2021 VAFB SLC-2W United StatesUnited States Spaceflight rideshare multiple satellites LEO
from 2022 several starts Template: future / in 2 years
Satlantis Earth observation satellites LEO
2Take-off mass of the payload including carried fuel ( wet mass ).
3Track height at which the payload is to be suspended; not necessarily the target orbit of the payload.

Firefly Beta and Lunar Lander

At least until the end of 2018, the beta only existed on paper. Before building it, Firefly wanted to focus on completing the Alpha. 2022–2023 was Template: future / in 2 yearsnamed as a possible period for an initial beta start .

In a first concept, this rocket resembled a Delta IV Heavy or Falcon Heavy : It should consist of three alpha first stages mounted next to each other and a second stage, which - unlike the Delta and Falcon - will be enlarged and strengthened. So the Beta should be 31 meters high and get a much larger payload section. For the second stage engine called Lightning 2 , 163 kN vacuum thrust was planned. The maximum take-off mass should increase to 150 tons, the payload capacity to 4000 kg LEO and 3000 kg SSO.

In connection with the Aeorjet-Rocketdyne cooperation, Firefly announced a complete overhaul of the beta design in October 2019. The two side boosters should be omitted, but the rest of the rocket will be significantly enlarged. A maximum payload of 8000 kg LEO and a reusability of the first stage are now aimed for. Instead of Reaver engines, Firefly is considering using the AR1 from Aerojet Rocketdyne for the first stage . According to the manufacturer, this engine generates approx. 2220  kN of thrust and was initially discussed for the large rocket Vulcan , before the manufacturer decided on the BE-4 from Blue Origin .

Firefly Aerospace is participating in the beta of NASA's Commercial Lunar Payload Services (CLPS) program launched in 2018 . As part of this program, the company can make offers to NASA for the launch of future moon landing devices. In July 2019, the company also announced the development of its own CLPS moon lander in cooperation with the Israeli aerospace company Israel Aerospace Industries (IAI). The technology developed for the Beresheet lander is to be used. A first moon landing is planned for the 4th quarter of 2021.

Firefly gamma

Firefly also presented a concept for a two-stage rocket plane called the Gamma . Like the space shuttle, it should take off vertically, but land as an airplane and be three-quarters of the way reusable. Optionally, take-offs from a carrier aircraft should also be possible. The main purpose is to launch small satellites, but cargo transports at hypersonic speeds are also conceivable.

Data table

alpha Beta (old) Beta (2019)
height  29.75 m 31 m > 31 m
Ø payload section  2.2 m 2.8 m
Drive first stage 
vacuum thrust 
motor starts 
4 × Reaver 1
736 kN
1
12 × Reaver 1
2208 kN
1
Drive second stage 
vacuum thrust 
motor starts 
1 × Lightning 1
70 kN
Up to 2
1 × Lightning 2
163 kN
Up to 2
Engine throttling  20-100%
Fuel / oxidizer  RP-1 / liquid oxygen
Tank pressure fluid  Heated helium
Takeoff mass  54.1 t 149.0 t
Max. Payload LEO  1000 kg 4000 kg 8000 kg
... 500 km SSE  630 kg 3000 kg
... GEO with kick stage      600 kg ?

Version 1.0 of the Payload User's Guide from August 2018 also specifies a trunk diameter of 1.8 meters.

Web links

Individual evidence

Unless otherwise stated, the certificates are in English.

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  46. Payload User's Guide. (PDF; 2.5 MB) Firefly Aerospace, August 10, 2018, accessed on May 12, 2019 .

Coordinates: 30 ° 32 '4.6 "  N , 97 ° 47" 59.2 "  W.