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  2. CFexpress - Wikipedia

    en.wikipedia.org/wiki/CFexpress

    The specification would be based on the PCI Express interface and NVM Express protocol. On 18 April 2017 the CompactFlash Association published the CFexpress 1.0 specification. [ 2 ] Version 1.0 will use the XQD form-factor (38.5 mm × 29.8 mm × 3.8 mm) with two PCIe 3.0 lanes for speeds up to 2 GB/s.

  3. NVM Express - Wikipedia

    en.wikipedia.org/wiki/NVM_Express

    NVM Express (NVMe) or Non-Volatile Memory Host Controller Interface Specification (NVMHCIS) is an open, logical-device interface specification for accessing a computer's non-volatile storage media usually attached via the PCI Express bus.

  4. EELV Secondary Payload Adapter - Wikipedia

    en.wikipedia.org/wiki/EELV_Secondary_Payload_Adapter

    The EELV Secondary Payload Adapter (ESPA) is an adapter for launching secondary payloads on orbital launch vehicles.. Originally developed for US launch vehicles in the 2000s to launch secondary payloads on space missions of the United States Department of Defense that used the Atlas V and Delta IV, the adapter design has become a de facto standard and is now also used for spaceflight missions ...

  5. List of solid-state drive manufacturers - Wikipedia

    en.wikipedia.org/wiki/List_of_solid-state_drive...

    Help; Learn to edit; Community portal; Recent changes; Upload file; Special pages

  6. Comparison of orbital rocket engines - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_orbital...

    Engine Origin Designer Vehicle Status Use Propellant Power cycle Specific impulse (s) [a] Thrust (N) [a] Chamber pressure (bar) Mass (kg) Thrust: weight ratio [b] Oxidiser: fuel ratio

  7. SABRE (rocket engine) - Wikipedia

    en.wikipedia.org/wiki/SABRE_(rocket_engine)

    Typical all-rocket systems peak around 450 seconds and even "typical" nuclear thermal rockets at about 900 seconds. The combination of high fuel efficiency and low-mass engines permits an SSTO approach, with air-breathing to Mach 5.14+ at 28.5 km (94,000 ft) altitude, and with the vehicle reaching orbit with more payload mass per take-off mass ...

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