being recovered after its
second flight Reusable spacecraft must survive reentry and safely return to the surface. The mass of any hardware dedicated for this reduces potential payload mass.
Atmospheric entry Orbital spacecraft initiate a deorbit burn and orient themselves for
atmospheric entry. The
Boeing Starliner and
Orion discard their service modules, including most of their maneuvering engines. The
SpaceX Dragon discards its trunk, which includes its solar panels and radiators, but retains its
Draco engines in the capsule. The Space Shuttle was notable for recovering the entire spacecraft. In general, around 15% of the landed weight of a vehicle is heat shielding.
Thermal protection systems (TPS) can be made of a variety of materials, including
reinforced carbon-carbon and
ablative materials. Historically, these materials were first developed on ballistic missile
reentry vehicles. However, the requirements of reusable space systems differ from those of single use reentry vehicles, especially with regards to heat shield requirements. In particular the need for durable high
emissivity coatings that can withstand multiple thermal cycles constitutes a key requirement in the development of new reusable spacecraft. Current materials for such high
emissivity coatings include transition metal disilicides. Ablative heat shields are reliable, but are heavy and diminished with use.
Reinforced carbon-carbon heat tiles such as those used on the Space Shuttle are fragile, which contributed to the
Columbia disaster. The Space Shuttle used the
LI-900 material.
Landing and refurbishment Runway landings from orbit became prevalent with the introduction of the
Space Shuttle. Spaceplanes that land horizontally on a runway require lifting surfaces and landing gear. Designs include the Space Shuttle's
delta wing and the
Dream Chaser's lifting body. Spaceplanes require access to a long enough runway, a necessary consideration for the Space Shuttle
launch abort modes. The first recoverable space capsules landed under parachute, either on land or by
splashing down in a body of water. Ground landings require additional cushioning, which
Starliner accomplishes with deployable airbags. This was considered for
Orion as well, but was ruled out due to the extra mass required. The sub-orbital
New Shepard uses retro-rockets to slow down just before touchdown, a technique that has been used by the expendable
Soyuz since the 1960s. Splashing down allows the water to cushion the spacecraft, but exposure to salt water can have adverse effects on the vehicle. Despite this, SpaceX began regularly reusing
Dragon capsules after splashdown.
Dragon 2 was originally designed to
propusively land using its
SuperDraco engines; however, propulsive landings for Dragon were canceled and Dragon 2 also uses parachutes to splashdown in the ocean.
Starship is designed to propulsively land using its
Raptor engines. It aims to be "caught" by the launch tower, as is done for the
Super Heavy booster. This eliminates the need for traditional landing legs on the vehicle and aims to lower the turnaround time between launches. After a spacecraft is recovered, it may need to be refurbished before its next flight. Depending on the spacecraft design, this process may be lengthy and expensive, and there may be a limit to how many times a spacecraft can be refurbished before it has to be retired. ==List of reusable spacecraft==