Suborbital Reusable Launch Vehicle (sRLV) Flight and Integration Services

Provide Suborbital Reusable Launch Vehicle (sRLV) services to fly Research and Development (R&D) technology payloads on platforms that provide reduced gravity or other relevant environments required to test technologies in order to advance their technology readiness. Services include:
*Reduced gravity with space environment - Requirement is to rapidly ascend from 0 km AGL to high altitude (typically 100km above ground level [AGL] or greater) and expose the payload to the low temperature and near-vacuum of space while simultaneously exposing the payload to very low values of gravity under stable gravitational conditions. This is typically accomplished by use of a sounding rocket or spacecraft.
*Slow ascent to high altitude with free-fall descent - Requirement is to expose payload to high altitude (typically 30 km AGL or greater) with a slow (typically 1 hour or greater) ascent and exposure to near-space environment followed by a descent to 0 AGL. This is typically accomplished by use of an untethered balloon with parachute descent.
*Rapid ascent to space environment with free-fall descent - Requirement is to attain high altitude (>100 km AGL) as rapidly as possible followed by a rapid free-fall descent to 0 km AGL. This is typically accomplished by use of a sounding rocket or spacecraft.
*Controlled descent with controlled vertical landing - Requirement is to descend from a minimum of 250 m AGL back to 0 AGL, under controlled rocket-powered flight and conduct a controlled vertical landing. Some payloads may require controlled horizontal translation of up to 1 km. Some applications may require allowing the payload to actively control portions of the flight profile. This is typically accomplished by use of a sounding rocket or spacecraft.
*Controlled vertical ascent and descent - Requirement is to rapidly ascend to high altitude (typically 30 km AGL or greater) along a pre-planned trajectory (typically vertical), hover in place, and then slowly descend back to 0 AGL under controlled conditions. This is typically accomplished by use of a sounding rocket or spacecraft.
*Contractors will be required to propose prices at the "by seat" level as well as the "full manifest" or both, as applicable. They will also be required to anticipate any common non-standard services required to integrate the technology payloads.