The Lynx will offer several multi-mission primary and secondary payload capabilities including: in-cockpit experiments, externally mounted experiments, test pilot/astronaut training, upper atmospheric sampling, microsatellite launch / ballistic trajectory research (Mk. III / US capability only), and personal spaceflight (space tourism). “Primary” payloads pay for the flight, while “secondary” payloads are on a ride-share basis with a primary payload, typically for a nominal ride-share fee.

Lynx vehicles will carry primary payloads located in the area to the right of the pilot or in the case of the Mk. III (US only) on the top of the vehicle in an experiment pod. Secondary payloads will be carried in a variety of locations. For the "Mk II" version of the Lynx, the primary internal payload will accommodate a maximum mass of 120 kg (265 lbs) to 100 km (330,000 ft). This “right seat” can be a human in a pressure suit, two stacked Space Shuttle middeck lockers (MDLs), or a standard 19 inch electronic equipment rack. For the US based Mk. III vehicle only, the primary payload location is an external dorsal mounted pod, which holds up to 650 kg (1433 lbs)and is large enough to hold a space telescope or a two stage carrier to launch multiple nanosatellites into low Earth orbit.  This pod can also carry experiments that return with the vehicle. Secondary payload spaces in all versions include a small area inside the cockpit behind the pilot or outside the vehicle in two areas in the aft fuselage fairing (see image below).  Detailed specifications of the payload spaces as well as information about engineering services and payload integration can be found in the Lynx Payload Users Guide.  Click here to apply for a copy.

<<< Development Plan | The Lynx Experience >>>