User manual MOOG SOFTRIDE BROCHURE

[. . . ] [. . . ] SoftRide has the capability to reduce dynamic responses of your spacecraft equipment by up to 50% and more, depending on the launch event. Imagine designing with reduced launch loads on optical components, batteries, tanks, struts, avionics, scientific equipment and more. The many benefits of implementing SoftRide include: SoftRide · Eliminating component requalification · Eliminating component redesign · Reducing launch loads on components · Reducing analysis time · Reducing design effort · Reducing weight of overdesigned structure · Reducing loads sensitivity to structural design changes · Eliminating workmanship level random vibe tests · Reducing expense · Decreasing risk FLIGHT PROVEN_ FLIGHT PROVEN_ Above Isolators Below Isolators Flight Data Showing Reduced Launch Loads SoftRide UniFlex (US Patent 6, 199, 801) · Designed to attenuate predominantly axial and bending loads · Reduces vibration, shock and structure-borne acoustics SoftRide OmniFlex (US Patent 7, 249, 756, EP Patent Pending) · Designed to attenuate axial, bending and lateral loads · Reduces vibration, shock and structure-borne acoustics SoftRide ShockRing (US Patent 6, 202, 961, EP 1 268 277) · Designed to attenuate shock loads · Reduces shock and structure-borne acoustics Flight heritage on Taurus, Pegasus, Minotaur I, Falcon I, Delta II, Delta IV Heavy, and Atlas V Suborbital Launch Vehicles. Compatible with and easily integrated onto all other launch vehicles. 2565 Leghorn Street, Mountain View, CA 94043-1613 USA +1. 650. 210. 9000 Fax: +1. 650. 210. 9001 www. moog-csa. com Form 500-704 0710 [. . . ] [. . . ]