System and method for deployment of space vehicle solar array

A method, comprising:

• deploying a system to a predetermined altitude,
• wherein the system comprises:
• a satellite;
• a first solar array,
• wherein the first solar array comprises at least a first solar panel;
• a second solar array,
• wherein the second solar array comprises at least a second solar panel;
• a boom having a first end and a second end opposite the first end,
• wherein the first end connects to the satellite;
• and
• a bracket assembly,
• wherein the bracket assembly comprise a first bracket, a second bracket, and a third bracket,
• wherein the first bracket connects the first solar array to the third bracket,
• wherein the first bracket comprises a first section and a second section,
• wherein the second section is angled relative to the first section, and
• wherein an angle between the first section and the second section is an acute angle,
• wherein the second bracket connects the second solar array to the third bracket, and
• wherein the third bracket connects the first bracket and the second bracket to the second end of the boom;
• and
• reorienting the first bracket and the second bracket, thereby to move the first solar array and the second solar array from a stowed position to a deployed position,
• wherein in the deployed position, the first and second solar arrays are oriented at a predetermined angle.