Orbital Space Flight

Shown below is our NOVA class family of orbital booster rockets. Adding booster sections provides for higher lift and/or extended mission capabilities.

The NOVA Booster

Both the NOVA Booster and NOVA/Silver Dart are launched from the Cape Breton Space Port in Nova Scotia. The NOVA family of rockets are to be mass-produced in Canada and the US, in facilities designed to accommodate the production of up to four launchers per month, with a capability to rapidly scale up to accommodate users' needs.

Payload Fairings

Depending on payload and mission requirements, PlanetSpace offers two types of payload fairings (see diagram below) Launcher type A, B, C payload fairing has an external diameter of 102 inches and a length of 287 inches. Launcher type C, D fairing with an external diameter of 144 inches and a length of 325 inches.

Typical Ascent Profile (with Dart upper stage)

Typical Ground Track for the First Three Stages

The Silver Dart is an autonomous and flexible hypersonic glider designed to operate as an orbital vehicle. It extends the capabilities of the booster to provide access to LEO. It is designed to double as an unmanned or manned spacecraft and can provide for a long duration platform in orbit. Based on the FDL-7 design which is stable in flight from Mach 22 to 0, the Silver Dart has the glide range of 25,000 miles (one earth circumference) with a cross range of over 4,000 miles. Such a glide performance provides for departure from any LEO and landing in the continental US with no wait time on orbit. An all metal thermal protection system allows for all weather flying. Combined, the thermal protection system and glide range result in a reentry vehicle that cannot be trapped in space and is able to return to base from any orbit around the Earth.

The FDL-7 began with the collaboration of Robert Masek of McDonnell Douglas and Alfred Draper of AFFDL in the late 1950s on hypersonic control issues. After a series of experimental and flight tests with different configurations the X tail configuration and the FDL-7C/D glider configurations emerged as the configuration that was inherently stable over the wide Mach range and had Earth circumferential glide.

With today’s automatic flight capability, visual requirements can be met with remote viewing systems. The modified FDL-7 C/D configuration was reshaped to have flat panel surfaces, and the windshield provisions were deleted, but it retains all of the essential FDL-7 characteristics.

It was a thoroughly designed and tested configuration with a complete all-metal thermal protection system that had the same weight of ceramic tile and carbon-carbon concepts used for the US Shuttle, but was sturdier. Crucial heat transfer tests on scale wind-tunnel models revealed that the sharp leading edges combined with a flat-bottomed, trapezoidal cross section drastically reduced the heating to the sides and upper surfaces.

The Silver Dart payload bay can be configured for either external cargo or internal cargo by interchanging a common payload module as shown on the next page.

A final manned version of this module will contain pilot control stations should the crew wish to switch to manual override. Both interior cargo and manned cargo modules are almost the same in design and operation with crew access through the rear docking tunnel.

All cargo manifests will be integrated with the cargo modules in a clean room and then sealed before installation into the Silver Dart. The modules contain power and equipment needed to preserve the integrity of the cargo.