Attachment Q - LandIS Simplified Mechanical Interface Control Drawing (MICD) Rev A.pdf

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Attached to
Landsat 10 Spacecraft
Solicitation number
80GSFC26R0015
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This is a Mechanical Interface Control Drawing (MICD) attachment for the Landsat 10 Landsat Instrument Suite (LandIS) component, issued under RFP 80GSFC26R0015 by NASA's Goddard Space Flight Center. The document is classified as "Landsat 10 Reviewed – Not Subject to Export Control" and serves as Attachment No. Q to the solicitation.

The MICD provides detailed technical specifications and dimensional drawings for the LandIS instrument's external interfaces, including mounting to the host spacecraft, center of mass location, fields of view, deployment swept volumes, and interfaces for instrument-mounted spacecraft components such as star trackers and inertial reference units. The document contains nine figures with scaled technical drawings showing interface fittings, dimensions in inches, NADIR and space cover rotation axes, and available volume specifications for IMSC (Instrument Mounted Spacecraft Component) integration. Key dimensional data includes specific interface fitting specifications, swept volume measurements for NADIR cover and space cover deployments, and available mounting volumes with precise coordinate measurements. The document was initially released on 03/24/2026 (Revision -) and updated on 06/30/2026 (Revision A) for the final RFP. This technical drawing serves as a reference specification for contractors responding to the Landsat 10 solicitation and defines the mechanical integration requirements for the LandIS instrument system.

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Attachment No. Q

LandIS Simplified Mechanical Interface Control Drawing

(MICD)

RFP 80GSFC26R0015

National Aeronautics and Space Administration Goddard Space Flight Center

LandIS Simplified MICD L10-LANDIS-ICD-0015 Rev A i Use or disclosure of data contained on this page is subject to the restriction(s) on the title page of this document.

CHANGE HISTORY LOG

Revision Effective Date Description of Changes Rev - 03/24/2026 Initial Release of Simplified Interface for SC RFP Rev A 06/30/2026 Updated Release of Simplified Interface for SC Final RFP

LandIS Simplified MICD L10-LANDIS-ICD-0015 Rev A ii Use or disclosure of data contained on this page is subject to the restriction(s) on the title page of this document.

TABLE OF CONTENTS

CHANGE HISTORY LOG ............................................................................................................. I TABLE OF CONTENTS ................................................................................................................ II

INTRODUCTION

List of Figures

Figure 1. LandIS Interfaces, Center of Mass Figure 2. LandIS Interfaces Figure 3. LandIS Fields of View Figure 4. LandIS Fields of View Figure 5. LandIS Deployments Swept Volume Figure 6. LandIS Deployments Swept Volume Figure 7. LandIS Instrument Mounted Spacecraft Component Mounting and Volume Figure 8. LandIS Instrument Mounted Spacecraft Component Mounting and Volume Figure 9. LandIS Instrument Mounted Spacecraft Component Available Volume

List of Tables

No table of figures entries found.

LandIS Simplified MICD L10-LANDIS-ICD-0015 Rev A

Use or disclosure of data contained on this page is subject to the restriction(s) on the title page of this document.

INTRODUCTION

The following figures show the external interfaces of the LandIS instrument, including the interface to the host spacecraft, center of mass, fields of view, deployment swept volume, and interface for instrument mounted spacecraft components (i.e. star trackers and inertial reference unit).

Use or disclosure of data contained on this page is subject to the restriction(s) on the title page of this document.

Figure 3. LandIS Fields of View

Use or disclosure of data contained on this page is subject to the restriction(s) on the title page of this document.

Figure 4. LandIS Fields of View

Use or disclosure of data contained on this page is subject to the restriction(s) on the title page of this document.

Figure 5. LandIS Deployments Swept Volume

Use or disclosure of data contained on this page is subject to the restriction(s) on the title page of this document.

Figure 6. LandIS Deployments Swept Volume

Use or disclosure of data contained on this page is subject to the restriction(s) on the title page of this document.

Figure 7. LandIS Instrument Mounted Spacecraft Component Mounting and Volume

Use or disclosure of data contained on this page is subject to the restriction(s) on the title page of this document.

Figure 9. LandIS Instrument Mounted Spacecraft Component Available Volume

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