Firm:

          

Exquadrum, Inc.

          

   

Address:

          

13313 Sabre Boulevard Suite 1, Victorville, CA 92394

          

   

Phone:

          

(760) 246-0279                                                                                                                                                                                

          

   

Name:

          

Elias Wilson

          

   

E-mail:

          

elias.wilson@exquadrum.com

          

   

Address:

          

13313 Sabre Blvd Ste 1, CA 92394 - 7903

          

   

Phone:

          

(760) 246-0279                                                                                                                                                                                

          

   

Name:

          

J. Mathew Jones

          

   

E-mail:

          

matt.jones@exquadrum.com

          

   

Address:

          

13313 Sabre Blvd Ste 1, CA 92394 - 2703

          

   

Phone:

          

(760) 246-0279                                                                                                                                                                                

          

   

Estimated Technology Readiness Level (TRL) :                                                                                                                                                          
Begin: 4
End: 6

          

          

     

Technical Abstract (Limit 2000 characters, approximately 200 words):

During the proposed Phase II research and development effort, the project team will integrate previously demonstrated technologies into a low-cost transfer stage based on a high energy density, aluminized, green monopropellant. The resulting stage will achieve the Mass Fraction and Specific Impulse performance needed to send small-spacecraft payloads in the near term to the cislunar environment, with longer term potential for farther destinations such as near-Earth objects, Mars, or Venus. The stage will be designed to provide support services to the spacecraft post-deployment, such as communications relay or positioning, navigation, and timing (PNT) services. The Phase I program will conclude with a hot-fire demonstration of the propulsion system.

          

          

     

Potential NASA Applications (Limit 1500 characters, approximately 150 words):

Small spacecraft transfer stage/upper stage propulsion systems for Small Launch Vehicles

          

          

     

Potential Non-NASA Applications (Limit 1500 characters, approximately 150 words):

Low cost space lift, exploration missions to the moon and Mars

          

          

     

Duration:     6