Indian Human Spaceflight Programme

Enlisted Spacecraft Experiments
10 January 2007: SRE-1

SRE-1
Space Capsule Recovery Experiment (SRE – 1) is a 550 kg capsule intended to demonstrate the technology of an orbiting platform for performing experiments in micro gravity conditions. After completion of the experiments, the capsule was de-orbited and recovered. SRE – 1 mission provided a valuable experience in fields like navigation, guidance and control during the re-entry phase, hypersonic aero thermodynamic, development of reusable thermal protection system (TPS), recovery through deceleration and flotation, besides acquisition of basic technology for reusable launch vehicles.
SRE – 1 carries two experiments, an Isothermal Heating Furnace (IHF) and a Bio-mimetic experiment. SRE was launched into a 635 km polar SSO in January 2007 as a co-passenger with CARTOSAT -2 and stayed in orbit for 10 days during which its payloads performed the operations they are intended to. The SRE capsule was de-boosted and recovered successfully back on earth on 22nd January 2007.
Launch Mass:
550 kg
Launch Vehicle:
PSLV-C7 / CARTOSAT-2 / SRE-1
Type of Satellite:
Science & Exploration
Manufacturer:
ISRO
Owner:
ISRO
Application:
Experimental
Orbit Type:
SSPO
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Crew module Atmospheric Re-entry Experiment (CARE)
Dec 18,2014
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Crew Module (CM) is identified as the payload in GSLV MK-III-X/CARE Mission. CARE is the acronym for Crew module Atmospheric Re-entry Experiment. The mission would be used as a platform for testing the re-entry technologies envisaged for Crew Module including validating the performance of parachute based deceleration system. CARE is expected to enhance the understanding of blunt body re-entry aerothermodynamics and parachute deployment in cluster configuration.
The external configuration of the Crew Module to be flight tested in GSLV MK-III is same as that of manned flight.

Objectives:
  • Demonstration of reentry flight of Crew Module
  • End to end parachute system validation
    • Demonstration of apex cover separation
    • Demonstration of parachute deployment
प्रमोचक राकेट / Launch Vehicle: LVM-3/CARE Mission
निर्माता / Manufacturer: ISRO
स्‍वामी / Owner: ISRO
अनुप्रयोग / Application: Experimental
The Crew Module (CM) is separated from the Launch Vehicle at an altitude of 126 km, re-enters Earth’s atmosphere at about 80 km and descends further in ballistic mode. Beyond 80 km, CM follows an uncontrolled re-entry trajectory and impacts at sea about 180 km from Andaman and Nicobar Island from where it will be recovered by Indian Coast guard.
 
Older Space Suit Concept from Sure Safety

View: https://youtu.be/92xvo_oTIgs
Suit features mentioned in above news clip:
  • Seven layered, fire-retardant, water-repellent, puncture-proof
  • Pressure controlled
  • Chilling water cooled
  • Umbilical connectors for suit-sensors, biometric sensors, air and oxygen supplies
  • Has approx 200 parts including mechanical, electrical and plastic parts
  • Weighs 13kg
  • Developed in 4 years
 
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Containers and Foods for Gaganyaan Crew

View: https://x.com/ANI/status/1214417678632251393
 

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