Vector-R

Vector-R
Function	Small satellite launch vehicle
Manufacturer	Vector Launch
Country of origin	United States
Cost per launch	2–3 million USD
Size
Height	12 m
Diameter	1.2 m
Mass	5,000 kg
Stages	2/3
Capacity
Payload to LEO
Mass	60 kg
Payload to SSO
Mass	26 kg
Associated rockets
Family	Vector (rocket family)
Derivative work	Vector-H
Comparable	Electron, Falcon 1, Firefly Alpha
Launch history
Status	Active
Launch sites	Mojave Air and Space Port; Spaceport Camden; Pacific Spaceport Complex – Alaska (planned); MARS Pad OB (planned); Spaceport Florida Launch Complex 46 (planned)
Total launches	2
Success(es)	2
Failure	0
First stage
Diameter	1.2 m (3 ft 11 in)
Powered by	3 X Hadley
Maximum thrust	15,000 lbf (67,000 N)
Propellant	Kerosene / LOX
Second stage
Diameter	.635 m (2 ft 1.0 in)
Powered by	1 X LP-2
Maximum thrust	1,000 lbf (4,400 N)
Burn time	433 seconds
Propellant	Propylene / LOX
	[edit on Wikidata]

Vector-R (Vector Rapid) is a two-stage orbital expendable launch vehicle under development by the American aerospace company Vector Launch to cover the commercial small satellite launch segment (CubeSats).^[3] Vector Launch went bankrupt in December 2019 and re-emerged in October 2020.^[4] Two prototypes were launched in 2017.

The rocket completed a maiden test flight at low altitude in May 2017.^[5] Vector Launch was planning the maiden orbital launch from the Pacific Spaceport Complex in Alaska in 2019,^[6] but paused operation in August 2019 due to an uncertain financing situation.^[7]

An upgraded version of the Vector-R, called the Vector-H (Heavy), is in development as well.

Design

Vector-R plans to use two stages with a 1.2-meter (3.9 ft) diameter first stage and 0.635-meter (2.08 ft) diameter second stage, both filled with propylene/LOX propellant. The main body of the rocket will be constructed using a lightweight carbon composite material.^[8]

The launch vehicle's first stage was to be powered by three LP-1 LOX/propylene engines, delivering 81,000 newtons of force. The second stage was to be powered by one LP-2 LOX/propylene engine, delivering 4,400 newtons of force. The engines used a 3D-printed engine injector, designed with help from NASA's Science, Technology and Mission Directorate (STMD) Flight Opportunities program. This allows the injector to be produced as a single piece of hardware, instead of as individual components.^{[citation needed]}

Vector was aiming the rocket at a launch cadence of 100 vehicles per year.^[9]

Block 0.1

The first two sub-orbital flight tests used the Vector-R Block 0.1 prototype model,^[10] which was a full size aluminum air-frame of the Vector-R but with only one first stage engine.

Vector-RE1

The Vector-RE1, a planned variant, was planned to use the same body as the standard Vector-R but include an electric powered third stage.^[10]

Intended usage

Vector-R was designed to launch a 60 kg (130 lb) payload to a 1,000 km (620 mi) Sun-synchronous orbit, suitable for CubeSats and other small satellites. The cost per launch was planned to be less than US$3 million, a price point that the company hoped would have allowed it to attract one hundred launches per year. Customers could have chosen to encapsulate their spacecraft in payload fairings provided by the company, which could be attached to the rocket shortly before launch, in several different configurations, such as fitting CubeSats dispensers or multiple satellites in a single fairing.

Vector used on-site payload integration for the early launches. However it was expected to be able to integrate payloads at their Arizona and California payload facilities and ship them to their launch sites.

Launch sites

Vector-R launched from the Mojave Air and Space Port and Spaceport Camden for its flight tests. It had completed one test flight from each pad. Flight B0.002 was also the first launch from Spaceport Camden.

Vector planned to use the LC-46 launch site in Florida and the Mid-Atlantic Regional Spaceport (MARS) Pad 0B^[11] for the Vector-R rocket, with the first all-up launches would have occurred from MARS Pad 0B.^[12] Additionally, Vector investigated adding more minimal infrastructure launch pads either located on land in the US, or to launch the rocket from barges on the ocean.^[2]

Vector had planned for the maiden orbital launch from Kodiak Spaceport Launch Complex earlier in 2019.^[13]

Launch statistics

Two low altitude suborbital test flights were performed in 2017.

Launch sites

0.5

1

1.5

2

2017

2018

2019

Launch outcomes

0.5

1

1.5

2

2017

2018

2019

2020

2021

2022

2023

Failure
Partial failure
Success
Scheduled

Launch history

Flight №	Date / time (UTC)	Rocket configuration	Launch site	Payload	Payload mass	Orbit	Customer	Launch outcome
B0.001	3 May 2017 19:00^[14]	Vector-R (P-19H)	Mojave^[15]	None	N/a	Sub-orbital	Vector Launch	Success
B0.001	Flight test; maiden flight of the Vector-R; first engineering test, scaled down version; scheduled altitude 4,500 feet (1,400 m).
B0.002^[16]	2 August 2017 16:15	Vector-R	Camden^[17]	Two customer payloads.		Sub-orbital	Astro Digital	Success
B0.002^[16]	Flight test; full prototype version, upgraded flight systems; the launch was delayed due to ignition detection failure; launch took place from a trailer; the peak altitude was about 5,000 ft (1,500 m).

Planned launches

Due to the bankruptcy and subsequent re-emergence of Vector, These launches are uncertain.

Date / time (UTC)	Rocket configuration	Launch site	Payload	Orbit	Customer
TBA	Vector-R	TBA	TBA	LEO?	TBA
TBA	B1001;^[18] First launch since re-emergence of bankruptcy.
TBA	Vector-R	Camden^[10]		Sub-orbital	Vector Launch
TBA	B0.003;^[19] Flight-Test; Testing fairings, avionics, and thrust vector control
TBA	Vector-R	PSCA^[20]	Unicorn 2A Delfi-PQ 1^[21]	LEO	Alba Orbital Delft University of Technology
TBA	First orbital and commercial flight of the Vector-R. PocketQube launch.
TBA	Vector-R	MARS LP-0B / PSCA	Landmapper-HD	LEO	Astro Digital
TBA	Earth observation
TBA	Vector-R				Open Cosmos
TBA

References

^ "Vector-R (Rapid)". Vector-launch.com. Archived from the original on 25 September 2018. Retrieved 27 October 2018.
^ ^a ^b "Vector-R : Payload User's Guide" (PDF). Vector-launch.com. Archived from the original (PDF) on 27 March 2018. Retrieved 27 October 2018.
^ "Vector Space Systems raises funds to develop small launch vehicle - SpaceNews.com". SpaceNews.com. 2016-04-26. Retrieved 2017-03-22.
^ "3. 2. 1. We're baaa-ack!".
^ "Vector has completed the first successful flight test of its new micro rocket". 2017-05-03. Retrieved 2017-05-04.
^ VECTOR (22 February 2018). "This week, Vector submitted its first launch application to the @FAANews to enable orbital launching from the Pacific Spaceport Complex - Alaska, later this year". @vectorspacesys. Retrieved 2018-02-25.
^ "Small satellite launcher Vector pauses operations after ousting CEO". 10 August 2019.
^ "Vector-R (Rapide) - Vector Space Systems". Vector Space Systems. Retrieved 2017-03-22.
^ "Tiny rocket company aims for 100 launches a year—and it just might succeed". Ars Technica. Retrieved 2017-03-22.
^ ^a ^b ^c "Vector". Space.skyrocket.de. Retrieved 27 October 2018.
^ "Vector to perform first orbital launches from Virginia". SpaceNews.com. 24 October 2017. Retrieved 27 October 2018.
^ Vector Space aims to expand launch ranges with minimal infrastructure pads NasaSpaceflight.com
^ VECTOR (22 February 2018). "This week, Vector submitted its first launch application to the @FAANews to enable orbital launching from the Pacific Spaceport Complex - Alaska, later this year". @vectorspacesys. Retrieved 2018-02-25.
^ "Vector Space Makes 1st Test Launch of Small-Satellite Rocket". Space.com. 3 May 2017. Retrieved 27 October 2018.
^ "Vector Becomes First to Complete Successful Flight Test of Launch Vehicle". PR Newswire. 3 May 2017. Retrieved 2017-11-11.
^ Vector. "Vector Successfully Launches First Ever Rocket from Spaceport Camden". www.prnewswire.com. Retrieved 27 October 2018.
^ Henning, Allyson (2 August 2017). "Camden Spaceport sees 1st launch". Jacksonville, FL: WJXT. Archived from the original on 2017-11-11. Retrieved 2017-11-11.
^ "11 Oct 22, Vector-R B1001. First mission soon". 11 October 2022. Retrieved 11 October 2022.
^ Cantrell, Jim (3 February 2018). "Our @vectorspacesys B0.003 vehicle being readied in our new factory in #Tucson for flight later in March testing multiple subsystems including fairings, avionics, and thrust vector control systems on a suborbital flight. Stay tuned !pic.twitter.com/54Nf3CwKiI". @jamesncantrell. Retrieved 2018-02-25.
^ "Vector planning first orbital launch this summer". SpaceNews.com. 20 February 2018. Retrieved 27 October 2018.
^ "Vector to Conduct Dedicated Launch of Alba Orbital PocketQube Satellites on First Orbital Attempt". PR Newswire. 8 March 2018. Retrieved 4 April 2018.

[1] "Vector-R (Rapid)". Vector-launch.com. Archived from the original on 25 September 2018. Retrieved 27 October 2018.

[vector-launch.com-2] "Vector-R : Payload User's Guide" (PDF). Vector-launch.com. Archived from the original (PDF) on 27 March 2018. Retrieved 27 October 2018.

[3] "Vector Space Systems raises funds to develop small launch vehicle - SpaceNews.com". SpaceNews.com. 2016-04-26. Retrieved 2017-03-22.

[4] "3. 2. 1. We're baaa-ack!".

[5] "Vector has completed the first successful flight test of its new micro rocket". 2017-05-03. Retrieved 2017-05-04.

[6] VECTOR (22 February 2018). "This week, Vector submitted its first launch application to the @FAANews to enable orbital launching from the Pacific Spaceport Complex - Alaska, later this year". @vectorspacesys. Retrieved 2018-02-25.

[operationstop-7] "Small satellite launcher Vector pauses operations after ousting CEO". 10 August 2019.

[8] "Vector-R (Rapide) - Vector Space Systems". Vector Space Systems. Retrieved 2017-03-22.

[9] "Tiny rocket company aims for 100 launches a year—and it just might succeed". Ars Technica. Retrieved 2017-03-22.

[skyrocket.de-10] "Vector". Space.skyrocket.de. Retrieved 27 October 2018.

[11] "Vector to perform first orbital launches from Virginia". SpaceNews.com. 24 October 2017. Retrieved 27 October 2018.

[12] Vector Space aims to expand launch ranges with minimal infrastructure pads NasaSpaceflight.com

[13] VECTOR (22 February 2018). "This week, Vector submitted its first launch application to the @FAANews to enable orbital launching from the Pacific Spaceport Complex - Alaska, later this year". @vectorspacesys. Retrieved 2018-02-25.

[14] "Vector Space Makes 1st Test Launch of Small-Satellite Rocket". Space.com. 3 May 2017. Retrieved 27 October 2018.

[15] "Vector Becomes First to Complete Successful Flight Test of Launch Vehicle". PR Newswire. 3 May 2017. Retrieved 2017-11-11.

[16] Vector. "Vector Successfully Launches First Ever Rocket from Spaceport Camden". www.prnewswire.com. Retrieved 27 October 2018.

[17] Henning, Allyson (2 August 2017). "Camden Spaceport sees 1st launch". Jacksonville, FL: WJXT. Archived from the original on 2017-11-11. Retrieved 2017-11-11.

[18] "11 Oct 22, Vector-R B1001. First mission soon". 11 October 2022. Retrieved 11 October 2022.

[19] Cantrell, Jim (3 February 2018). "Our @vectorspacesys B0.003 vehicle being readied in our new factory in #Tucson for flight later in March testing multiple subsystems including fairings, avionics, and thrust vector control systems on a suborbital flight. Stay tuned !pic.twitter.com/54Nf3CwKiI". @jamesncantrell. Retrieved 2018-02-25.

[20] "Vector planning first orbital launch this summer". SpaceNews.com. 20 February 2018. Retrieved 27 October 2018.

[21] "Vector to Conduct Dedicated Launch of Alba Orbital PocketQube Satellites on First Orbital Attempt". PR Newswire. 8 March 2018. Retrieved 4 April 2018.

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v t e Orbital launch systems developed in the United States
Active	Atlas V**^†† Electron Falcon 9 Block 5 Falcon Heavy Firefly Alpha Minotaur I IV V C New Glenn Pegasus XL SLS Block 1 Vulcan Centaur
In development	Antares 330 Daytona I Eclipse Neutron Nova Red Dwarf SLS Block 1B Block 2 Starship Terran R
Retired	Antares 110/120/130/230/230+^††† Athena I II Atlas B D E/F G H I II III LV-3B SLV-3 Able Agena Centaur Conestoga^† Delta A B C D E G J L M N 0100 1000 2000 3000 4000 5000 II III IV IV Heavy Falcon 1 Falcon 9 v1.0 v1.1 v1.2 "Full Thrust" H-I* Juno I Juno II LauncherOne N-I* N-II* Pilot^† Rocket 3 RS1^† Saturn I IB V Scout Space Shuttle SPARK^† Sparta Terran 1^† Thor Able Ablestar Agena Burner Delta DSV-2U Thorad-Agena Titan II GLV IIIA IIIB IIIC IIID IIIE 34D 23G CT-3 IV Vanguard
* - Japanese projects using US rockets or stages ** - uses Russian engines ^† - never succeeded ^†† - no new orders accepted and production stopped ^††† - used Ukrainian first stage

v t e Orbital launch systems
List of orbital launch systems Comparison of orbital launch systems
Current	Angara 1.2 A5 Ariane 6 Atlas V Ceres 1 1S 2^† Chollima-1 Electron Eris^† Falcon 9 Block 5 Falcon Heavy Firefly Alpha Gravity-1 GSLV H3 HANBIT-NANO^† Hyperbola-1 Jielong 1 3 KAIROS^† Kaituozhe 2 Kinetica 1 2 Kuaizhou 1 1A 11 Long March 2C 2D 2F 3A 3B/E 3C 4B 4C 5 5B 6 6A 6C 7 7A 8 11 11H 12 12A LVM3 Minotaur I IV V C New Glenn Nuri OS-M1^† Pegasus XL Proton-M PSLV Qaem 100 Qased Shavit 2 Simorgh SLS Block 1 Soyuz-2 2.1a / STA 2.1b / STB Spectrum^† SSLV Starship Tianlong 2 3^† Unha Vega C Vulcan Centaur Zhuque 2E 3
In development	Antares 330 Bloostar Blue Whale 1 Cyclone-4M Deca Eclipse Epsilon S Gravity-2 Hyperbola-2 Irtysh Kinetica 2H 3 KSLV-III Kuaizhou 21 31 Long March 9 10 Miura 5 Neutron New Line 1 NGLV Nova OS-M 2 4 Pallas-1 Red Dwarf RFA One SLS Block 1B Block 2 Soyuz-7 Terran R VLM Vega E Zero Zuljanah
Retired	Antares 110 120 130^† 230 230+ Ariane 1 2 3 4 5 ASLV Athena I II Atlas B D E/F G H I II III LV-3B SLV-3 Able^† Agena Centaur Black Arrow Conestoga^† Delta A B C D E G J L M N 0100 1000 2000 3000 4000 5000 II III IV IV Heavy Diamant Dnepr Energia Epsilon Europa I^† II^† Falcon 1 Falcon 9 v1.0 v1.1 v1.2 "Full Thrust" Feng Bao 1 GSLV Mk I H-I H-II H-IIA H-IIB Juno I Juno II Kaituozhe-1 Kosmos original 1 2/2I 3 3M Lambda 4S LauncherOne Long March 1 1D^† 2A 2E 3 3B 4A Mu 4S 3C 3H 3S 3SII V N1^† N-I N-II Naro-1 Paektusan^† Pilot-2^† R-7 Luna Molniya M L Polyot Soyuz original FG L M U U2 2-1v Soyuz/Vostok Sputnik Voskhod Vostok L K 2 2M R-29 Shtil' Volna^† Rocket 3 RS1^† Safir 1 1A 1B Saturn I IB V Scout X-1 Blue Scout II^† X-2^† X-2M X-3 X-3M X-4 X-2B^† B A B-1 D-1 A-1 E-1 F-1 G-1 Shavit original 1 SLV Space Shuttle SPARK^† Sparta SS-520 Start-1 Terran 1^† Thor Able Ablestar 1 2 Agena A B D Burner 1 2 Delta DSV-2U Thorad-Agena SLV-2G SLV-2H Titan II GLV IIIA IIIB IIIC IIID IIIE 34D 23G CT-3 IV Tsyklon R-36-O original 2 3 Universal Rocket UR-500 Proton Proton-K Rokot Strela Vanguard Vega original VLS-1^† Zenit 2 2M 2FG 3SL 3SLB 3F Zhuque 1^† 2
Classes	Sounding rocket Small-lift launch vehicle Medium-lift launch vehicle Heavy-lift launch vehicle Super heavy-lift launch vehicle
This template lists historical, current, and future space rockets that at least once attempted (but not necessarily succeeded in) an orbital launch or that are planned to attempt such a launch in the future Symbol ^† indicates past or current rockets that attempted orbital launches but never succeeded (never did or has yet to perform a successful orbital launch)

Vector-R

Design

Block 0.1

Vector-RE1

Intended usage

Launch sites

Launch statistics

Launch sites

Launch outcomes

Launch history

Planned launches

See also

References