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This document describes the format and specifications for the Mars Reconnaissance Orbiter's MARCI Standard Data Product, including data handling and processing methods.
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How to fill out Mars Reconnaissance Orbiter Software Interface Specification

01
Start by opening the Mars Reconnaissance Orbiter Software Interface Specification document.
02
Read the introduction to understand the purpose and scope of the specification.
03
Familiarize yourself with the terminology used within the document.
04
Identify the sections relevant to your software application.
05
Fill out each section according to the guidelines provided in the document.
06
Pay special attention to the requirements and performance metrics.
07
Review any examples provided in the specification to ensure clarity.
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Who needs Mars Reconnaissance Orbiter Software Interface Specification?

01
Software developers working on Mars Reconnaissance Orbiter projects.
02
Project managers overseeing the development of software for the mission.
03
System engineers involved in integrating software with hardware components.
04
Quality assurance teams responsible for testing the software.
05
Stakeholders interested in understanding software requirements and specifications.
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As of April 28, 2025, the MRO has been active at Mars for 6802 sols, or 19 years, 1 month and 18 days, and is the third longest-lived spacecraft to orbit Mars, after 2001 Mars Odyssey and Mars Express.
Subtracting Mars's radius gives an orbital altitude of 17,032 km (10,583 mi). Two stable longitudes exist - 17.92°W and 167.83°E.
Propulsion is provided by a total of 20 thrusters. Six 170 N (Newton) monopropellant (hydrazine) main-engine thrusters are used for the Mars Orbit insertion burn, a maneuver which will require about 70% of the total fuel onboard.
CTX makes observations simultaneously with high-resolution images collected by HiRISE and data collected by the mineral-finding CRISM spectrometer. <br>CTX provides the wider context for the data collected by the other two instruments.
Six 170 N (Newton) monopropellant (hydrazine) main-engine thrusters are used for the Mars Orbit insertion burn, a maneuver which will require about 70% of the total fuel onboard. Six 22 N thrusters are used for trajectory correction maneuvers and eight 0.9 N thrusters for pointing.
Through these efforts, MRO has found that Mars experienced many geologic processes similar to the ones that shaped Earth in its past, including volcanic lava flows, wind erosion forming massive buttes, the depositing of sedimentary layers within lake beds, and meandering rivers cutting through bedrock.
MRO utilizes a three-axis stabilized Attitude Control System (ACS) that relies on star trackers, Sun sensors, an Inertial Measurement Unit (IMU), and a Reaction Wheel Assembly (RWA) for attitude control. The spacecraft attitude measurements are provided via star trackers and Sun sensors.
MRO began orbital insertion by approaching Mars on March 10, 2006, and passing above its southern hemisphere at an altitude of 370–400 kilometers (230–250 miles).

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The Mars Reconnaissance Orbiter Software Interface Specification defines the protocols and standards required for software interaction with the Mars Reconnaissance Orbiter's systems, providing guidelines for compatibility and functionality.
Individuals and organizations developing software intended to interact with the Mars Reconnaissance Orbiter are required to file the software interface specification to ensure compliance with mission requirements.
To fill out the Mars Reconnaissance Orbiter Software Interface Specification, developers must follow the provided template and guidelines, ensuring all sections are completed with relevant information pertaining to software functionality, integration, and performance criteria.
The purpose of the Mars Reconnaissance Orbiter Software Interface Specification is to ensure interoperability between different software systems and the orbiter, facilitating seamless communication and operation for mission success.
The Mars Reconnaissance Orbiter Software Interface Specification must report information including software architecture, data formats, communication protocols, operational procedures, and performance metrics to ensure compatibility and effective operation.
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