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Rocket Lab Electron launches "Don't Be Such a Square" Mission

STP-S30 is a complex mission that will deliver research experiments and technology demonstrations to orbit for the DoD and contribute to future space systems development. The primary payload, DiskSat, will demonstrate sustained very low earth orbit (VLEO) flight and test a unique, 1-meter diameter, disk-shaped satellite bus that is designed …

Don't Be Such A Square (STP-S30)

Circle Image

Overview

Destination: Low Earth Orbit
Mission: Technology

Low Earth Orbit Rocket Lab Launch Complex 2 (Launch Area 0 C) Wallops Flight Facility, Virginia, USA Probability: 80%

STP-S30 is a complex mission that will deliver research experiments and technology demonstrations to orbit for the DoD and contribute to future space systems development. The projected primary payload, DISKSat, will demonstrate sustained very low earth orbit (VLEO) flight and test a unique, 1-meter diameter, disk-shaped satellite bus that is designed to increase on-orbit persistence.

Telemetry

Launch trajectory and telemetry simulations provided by Flight Club - a rocket launch simulator and orbital trajectory visualiser for all things space!

Updates

Cosmic_Penguin • Aug. 11, 2025, 12:12 p.m.

NET late 2025.


Cosmic_Penguin • Dec. 16, 2025, 11:06 p.m.

GO for launch.


Cosmic_Penguin • Oct. 25, 2025, 9:57 p.m.

NET December 8.


Cosmic_Penguin • Dec. 10, 2025, 10:07 p.m.

GO for launch (launch window is per https://forum.nasaspaceflight.com/index.php?topic=63362.msg2742010#msg2742010).


Cosmic_Penguin • Dec. 18, 2025, 2:13 a.m.

Updated launch weather, 70% GO.


Electron

Family:
Configuration:

Electron is a two-stage orbital expendable launch vehicle (with an optional third stage) developed by the American aerospace company Rocket Lab. Electron is a small-lift launch vehicle designed to launch small satellites and cubesats to sun-synchronous orbit and low earth orbit. The Electron is the first orbital class rocket to use electric-pump-fed engines, powered by the 9 Rutherford engines on the first stage. It is also used as a suborbital testbed (called HASTE) for hypersonics research.

See Details
Specifications
  • Minimum Stage
    2
  • Max Stage
    3
  • Length
    18.0 m
  • Diameter
    1.2 m
  • Fairing Diameter
    1.2 m
  • Launch Mass
    13.0 T
  • Thrust
    162.0 kN
Family
  • Name
    Electron
  • Family
  • Variant
  • Alias
  • Full Name
    Electron
Payload Capacity
  • Launch Cost
    $6000000
  • Low Earth Orbit
    300.0 kg
  • Geostationary Transfer Orbit
  • Direct Geostationary
  • Sun-Synchronous Capacity
    225.0 kg

Rocket Lab

Rocket Lab

(RL)

CEO: Peter Beck Founded: 2006 Successes: 87 Failures: 4 Pending: 43

Agency Type:

Rocket Lab is an American aerospace manufacturer with a wholly owned New Zealand subsidiary. The company develops lightweight, cost-effective commercial rocket launch services. The Electron Program was founded on the premise that small payloads such as CubeSats require dedicated small launch vehicles and flexibility not currently offered by traditional rocket systems. Its rocket, the Electron, is a light-weight rocket and is now operating commercially. The company is also producing a variety of spacecrafts and spacecrafts components.

INFO WIKI

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Wallops Flight Facility, Virginia, USA

Rocket Lab Launch Complex 2 (Launch Area 0 C)


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