Engineered to interface between the launch vehicle structure and payloads, the TULIP solution integrates all essential elements into one cohesive design. With a payload fairing envelope diameter of approximately 2 meters, the Tulip provides various configuration options, making it the perfect choice for diverse mission requirements.

The TULIP ‘s design can include up to six modular petals, each capable of housing microsatellites or deployers. Additionally, its central hub provides an option to attach a microsatellite, maximizing payload efficiency and making optimal use of the available space. For smaller missions, petals can be removed, offering a fully customizable solution to meet your payload configuration needs.

With its versatile and innovative design, the Tulip delivers a reliable and efficient solution for payload integration, ensuring every mission is a success.

Product Specification

Mass*

Two petals: ~38 kg (estimate)
Four petals: 70.1 kg
Six petals: ~100 kg (estimate)

*depends on petal type selection

Payload fairing envelope diameter

~ 2m

Interface to LV

36x D24” thread holes

Interface to payload

Central Module: 24x D15” or
12x D8” thread holes
Petals Module: 24x D15” or
12x D8” thread holes as well as deployer interface

Qualification and Acceptance Testing

QT

Is performed on the design/qualification model

AT

Is performed on the unit to be shipped

Functional Test Unchecked Unchecked
Thermal Vacuum Unchecked Unchecked
Thermal Cycling Unchecked Unchecked
Vibration Test Checked Checked
Mechanical Shock Unchecked Unchecked
1
Missions Flown

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