LM 400

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Description

Lockheed Martin Space encourages payload providers and mission planners to create missions optimized for – or at least compatible with – our versatile and highly capable LM 400 LEO/GEO Small Satellite platform. Table 1 provides a summary of typical interfaces and performance capabilities provided by the LM 400 platform. These specifications serve as a guide to those interested in flying on this bus. An actual compatibility assessment is best done through an exchange of detailed information and interface requirements, as the LM 400 is quite flexible in configuration and capability. Figure 1 shows a nominal payload volume for an externally mounted payload with internal electronics, if required. In many cases, specific interface adaptations are easily accommodated.

 

Datasheet

Lockheed Martin – LM 400

Overview
NameLM 400
ManufacturerLockheed Martin
SubsystemBus
ClassificationSmallSat
Lead Time24 to 30 Months
Vendor Overview
Vendor NameLockheed Martin
Vendor Websitehttps://www.lockheedmartin.com/en-us/index.html
Vendor LocationsAustralia, Canada, Chile, Germany, India, Israel, Japan, Korea, Poland, Puerto Rico, Qatar, Saudi Arabia, Singapore, United Arab Emirates, United Kingdom, United States
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SPECIFICATIONS
SubsystemBus
ClassificationSmallSat
VendorLockheed Martin
HeritageN/A
Mass600.0 kg

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